<table>
<colgroup>
<col style="width: 7%" />
<col style="width: 5%" />
<col style="width: 13%" />
<col style="width: 4%" />
<col style="width: 5%" />
<col style="width: 13%" />
<col style="width: 13%" />
<col style="width: 8%" />
<col style="width: 9%" />
<col style="width: 10%" />
<col style="width: 5%" />
<col style="width: 2%" />
</colgroup>
<thead>
<tr class="header">
<th colspan="8"><h1 id="payload-flight-hazard-report">PAYLOAD FLIGHT
HAZARD REPORT</h1></th>
<th>a. NO:</th>
<th colspan="3">AMS-02-F01</th>
</tr>
<tr class="odd">
<th colspan="2">b. PAYLOAD</th>
<th colspan="6">Alpha Magnetic Spectrometer-02 (AMS-02)</th>
<th>c. PHASE:</th>
<th colspan="3">II</th>
</tr>
</thead>
<tbody>
<tr class="odd">
<td colspan="2">d. SUBSYSTEM:</td>
<td colspan="3">Structures</td>
<td>e. HAZARD GROUP:</td>
<td colspan="2">Collision, Injury</td>
<td>f. DATE:</td>
<td colspan="3">May 25, 2007</td>
</tr>
<tr class="even">
<td colspan="2" rowspan="2">g. HAZARD TITLE:</td>
<td colspan="6" rowspan="2">Structural Failure of Hardware</td>
<td>i. HAZARD</td>
<td colspan="2">CATASTROPHIC</td>
<td><strong>X</strong></td>
</tr>
<tr class="odd">
<td>CATEGORY:</td>
<td colspan="2">CRITICAL</td>
<td></td>
</tr>
<tr class="even">
<td colspan="4">h. APPLICABLE SAFETY REQUIREMENTS:</td>
<td colspan="8">NSTS 1700.7B and the ISS Addendum, 200.2, 208.1, 208.2,
208.3</td>
</tr>
<tr class="odd">
<td colspan="4">j. DESCRIPTION OF HAZARD:</td>
<td colspan="8">Failure of AMS-02 Structures could injure crewmembers or
damage the STS, ISS or other payloads. This hazard does not address
non-structural pressure systems or sealed/vented container
failures.</td>
</tr>
<tr class="even">
<td>k. CAUSES</td>
<td colspan="11" rowspan="2"><blockquote>
<p>1. Inadequate structural strength for worst-case loads during all
mission phases.</p>
<p>2. Improper Material Selection (including Stress Corrosion
Cracking)</p>
<p>3. Initiation of propagation of flaws or crack-like defects.</p>
<p>4. Use of counterfeit, substandard or inadequate fasteners.</p>
<p>5. Loosening of safety critical fasteners.</p>
<p>6. Loss of structural integrity of welds.</p>
<p>7. Improper manufacture and/ or assembly.</p>
<p>8. Improper preload or creeping of the Cryomagnet support system
straps.</p>
<p>9. Damage to composite structural components during manufacturing,
assembly operations, ground handling, and/or ground transportation.</p>
<p>10. Degradation of composite structural components by atomic
oxygen.</p>
<p>11. Improper Preload of PAS</p>
<p>12. Reconfiguration of Mechanical Components</p>
</blockquote></td>
</tr>
<tr class="odd">
<td><em>(list)</em></td>
</tr>
<tr class="even">
<td colspan="12"></td>
</tr>
<tr class="odd">
<td colspan="3">o. APPROVAL</td>
<td colspan="4">PAYLOAD ORGANIZATION</td>
<td colspan="5">SSP/ISS</td>
</tr>
<tr class="even">
<td colspan="3">PHASE I</td>
<td colspan="4"></td>
<td colspan="5"></td>
</tr>
<tr class="odd">
<td colspan="3">PHASE II</td>
<td colspan="4"></td>
<td colspan="5"></td>
</tr>
<tr class="even">
<td colspan="3">PHASE III</td>
<td colspan="4"></td>
<td colspan="5"></td>
</tr>
<tr class="odd">
<td colspan="12"></td>
</tr>
<tr class="even">
<td colspan="10">l. HAZARD CONTROL (CONTROL), m. SAFETY VERIFICATION
METHODS (SVM), n. STATUS OF VERIFICATIONS (STATUS)</td>
<td colspan="2">OPS CONTROL</td>
</tr>
<tr class="odd">
<td colspan="10">1. CAUSE: Inadequate structural strength for worst-case
loads during all mission phases. These loads include, but are not
limited to: differential temperature, thermal extremes, differential
pressure, depressurization and repressurization, acoustics, sloshing of
SFHe, ground transportation and handling, on-orbit (including transfer
operations from the Orbiter to the ISS and crew induced) and magnet
forces.</td>
<td colspan="2"></td>
</tr>
<tr class="even">
<td colspan="10"><p>1.1 CONTROL: The AMS-02 hardware is being designed
to have positive margins of safety during all mission phases (Note
exception in Control 1.4). All metallic structures will be tested or
analyzed to show margin to the appropriate factors of safety (FOS). For
testing the margin will be shown to a 1.0 FOS to yield, 1.4 FOS to
ultimate. For analyzed structures the margin will be shown to a 1.25 FOS
to yield, 2.0 FOS to ultimate. Non-metallic structures will be
tested/analyzed to 1.25 FOS (yield), 2.0 FOS (ultimate). For ISS mission
phases factors of safety of 1.5 ultimate and 1.1 for yield are used for
metallic structures, 2.0 ultimate and 1.2 proof (1.4 for launch) for
composite structures. In all cases all items have been analyzed to
Shuttle and ISS on-orbit loads and results documented in AMS-02
Structural Verification Plan. (Note: Any exceptions to this control are
documented in Control 1.4) Attached Table indicates FOS used and margins
for structural components.</p>
<p>1.1.1 SVM: Review and approval of the AMS-02 Structural Verification
Plan (SVP) (JSC 28792), which includes the requirements in NSTS 14046,
by the JSC Structures Working group (SWG). Individual test plans derived
from the SVP will be reviewed and approved by the JSC SWG.</p>
<p>1.1.2 SVM: Structural analysis will be performed to the appropriate
factors of safety for all load conditions. Review and approval of the
AMS-02 Structural Analysis Reports by the JSC SWG.</p>
<p>1.1.3 SVM: Static strength and strength model verification tests for
the all-up configuration of the AMS-02 payload will be performed. Review
and approval of the AMS-02 Static Correlation Report by the JSC SWG.</p>
<p>1.1.4 SVM: Model Correlation. Modal test on the all-up configuration
of the AMS-02 payload and sine sweep test of the Structural Test Article
(STA) will be performed for dynamic math model verification. Review and
approval of the AMS-02 Modal Correlation Report and STA Sine Sweep
Correlation Report by the JSC SWG.</p>
<p>1.1.5 SVM: Buckling analyses of the Cryomagnet Vacuum Case (VC) will
be performed. Review and approval of the Cryomagnet VC Buckling Analyses
by the JSC SWG.</p>
<p>1.1.6 SVM: Proof pressure test of the Cryomagnet Flight VC and the
Structural Test Article (STA) VC will be performed. Review and approval
of the Cryomagnet Flight VC and STA VC Proof Pressure Test Report by the
JSC SWG.</p>
<p>1.1.7 SVM: An operating test of the Cryomagnet to 1.1 times the limit
load will be performed. Review and approval of the Cryomagnet Operating
Test Plan and Test Report by the JSC SWG.</p>
<p>1.1.8 SVM: Qualification, acceptance, fatigue and development static
and dynamic tests on the Cryomagnet support system straps will be
performed. Review and approval of the Cryomagnet Support System Straps
Verification Test Plans and Test Reports by the JSC SWG.</p>
<p>1.1.9 SVM: Acoustic analysis of the TRD, TOF, TCS and Si Tracker has
been performed (other items are not acoustic receivers). Acoustic test
of the STA VC will be performed. Review and approval of the Acoustic
Analyses, Acoustic Test Plan and Acoustic Test Report by the JSC
SWG.</p>
<p>1.1.10 SVM: Sine sweep, "smart -hammer" or modal testing, or analysis
(by subsystem) will be performed to verify the first natural frequency
of any secondary structure with a global mode that is below 50 Hz.
Review and approval of the Sine Sweep, "Smart -Hammer" or Modal Test
Plan, analysis methodology (part of the SVP) and Test Report by the JSC
SWG.</p>
<p>1.1.11 SVM: Static verification tests of the Payload Attach System
(PAS) and Interface Verification Test (IVT) of the PAS to ISS S3 Zenith
Inboard Active PAS 2 were performed. Review and approval of the Static
Test Report and IVT verification memorandum by the ISS Structures
Team.</p>
<p>1.1.12 SVM: Other subdetector items in the AMS-02 SVP will be
verified by letters of certification per SVP.</p>
<p>1.1.1 STATUS: Closed. SWG approval documented in memorandum
ES2-06-003, “Alpha Magnetic Spectrometer-02 Structural Verification
Plan, JSC-28792 Rev. D” date January 31, 2006.</p>
<p>1.1.2 STATUS: Open. Most of Analysis is Complete, formal documents in
work</p>
<p>1.1.3 STATUS: Open. Static testing of full payload currently
scheduled for June 2007</p>
<p>1.1.4 STATUS: Open. Sine sweep test of STA VC conducted January 2007,
report pending. Modal testing of full payload currently scheduled for
July 2007.</p>
<p>1.1.5 STATUS: Open. Nonlinear analysis presented and approved by SWG,
formal documentation in work.</p>
<p>1.1.6 STATUS: Open. Test of STA VC Complete, test of Flight VC
scheduled for 1<sup>st</sup> quarter 2008.s</p>
<p>1.1.7 STATUS: Open</p>
<p>1.1.8 STATUS: Open . 1-D dynamic test, warm static test, cold static
test, and fatigue test complete. Initial 1-D dynamic test report
(LMSEAT-34044), warm static test report (MSAD-04-0054), Cold static test
report and fatigue test report (CTG-SCL-290802) under review by SWG.
Follow-on 1-D dynamic test report in work.</p>
<p>1.1.9 STATUS: Open. Acoustic analysis of the TCS and TRD complete,
formal documentation in work. Acoustic analysis of the TOF, RICH, and
Tracker in work. Full VC acoustic test currently scheduled for February
2006.</p>
<p>1.1.10 STATUS: Open. Current testing requirements for each
substructure defined in SVP. The ECAL did a sine sweep test to verify
the first mode of the ECAL is 51.8 Hz. Documentation is still in work.
The TOF, TRD, and TCS groups have dynamic tests scheduled. Other groups
have provided FEM results demonstrating first modes well above the 50 Hz
requirement.</p>
<p>1.1.11 STATUS: Closed. PAS Static Test Plan (LMSEAT 34105) reviewed
and approved by ISS Structures and Mechanisms Team. IVT Test Preparation
Sheet (BCP-S3-T037), PAS Test Report (53103), and IVT Test Report
(53103A) provided to ISS Structures and Mechanisms Team for review.</p>
<p>1.1.12 STATUS: Open</p></td>
<td colspan="2"></td>
</tr>
<tr class="odd">
<td colspan="10"><p>1.2 CONTROL: SFHe tank feed through tubes are
designed to physically isolate the Cryomagnet support system straps from
bending, lateral or torsional loads. The Cryomagnet support system
straps carry only axial loads.</p>
<p>1.2.1 SVM: Structural analysis will show that there is adequate
clearance between the strap and the tube to prevent transfer of loads to
the straps.</p>
<p>1.2.1 STATUS: Open. Adequate strap clearance demonstrated in latest
DCLA. Clearance will continue to be monitored through the Verification
Loads Analysis based on final measured static clearances.</p></td>
<td colspan="2"></td>
</tr>
<tr class="even">
<td colspan="10"><p>1.3 CONTROL: EVA Sites and translation paths have
been assessed for compatibility with EVA contact loads, specifically EVA
kick loads of 125 pounds. All structures that can be contacted have been
assessed to have a positive margin considering a factor of safety of
2.0.</p>
<p>1.3.1 SVM: Structural Analysis</p>
<p>1.3.1 STATUS: Open</p></td>
<td colspan="2">`</td>
</tr>
<tr class="odd">
<td colspan="10"><p>1.4 CONTROL: Structural joints, junctions of
structural members, that fail to attain a positive margin to the
required factors of safety have been presented to the Structures Working
Group and individually assessed for acceptability on the specific
application and fracture acceptance rationale. The concern is that these
joints can experience joint separation during the most severe loading
conditions and while the joint fasteners are not yielding or losing
structural integrity, the joint may experience excessive load cycles
that impact the overall fracture control acceptability of the hardware.
The AMS-02 will document and present to the Structures Working Group
analyses that demonstrate the loading cycles that these joints will
experience will not pose a risk to the overall hardware integrity or
load carrying capability. NOTE: This control does not address any
structural members as having negative margins, only the interface of
some structural members at interconnecting joints.</p>
<p>1.4.1 SVM: Acceptance of all occurrences of negative margins
(documented in Stress Report) on joints by the JSC Structures Working
Group.</p>
<p>1.4.1 STATUS: Open</p></td>
<td colspan="2"><mark></mark></td>
</tr>
<tr class="even">
<td colspan="10">2. CAUSE: Improper Material Selection (including Stress
Corrosion Cracking)</td>
<td colspan="2"></td>
</tr>
<tr class="odd">
<td colspan="10"><p>2.1 CONTROL: AMS-02 materials will be selected to
meet the requirements of MSFC-STD-3029. Materials with high resistance
to stress corrosion cracking will be used where possible. Materials with
moderate or low resistance to stress corrosion cracking have MUAs that
have been/will be approved for each application. Identified materials to
be covered in MUAs are attached to this hazard report.</p>
<p>2.1.1 SVM: Stress Corrosion Evaluation of materials list and
drawings.</p>
<p>2.1.2 SVM: ES4/Material and Processes Branch Certification for
materials usage.</p>
<p>2.1.1 STATUS: Open</p>
<p>2.1.2 STATUS: Open</p></td>
<td colspan="2"></td>
</tr>
<tr class="even">
<td colspan="10"><p>2.2 CONTROLS: Joints and junctions of dissimilar
metals will be avoided and where they cannot be avoided the materials
will be selected to reduce the potential for galvanic corrosion.</p>
<p>2.2.1 SVM: Material Compatibility Assessment</p>
<p>2.2.2 SVM: Approval of material use and MUAs by JSC ES4/Materials and
Processes Branch</p>
<p>2.2.1 STATUS: Open</p>
<p>2.2.2 STATUS: Open</p></td>
<td colspan="2"></td>
</tr>
<tr class="odd">
<td colspan="10">3. CAUSE: Initiation or propagation of flaws or
crack-like defects.</td>
<td colspan="2"></td>
</tr>
<tr class="even">
<td colspan="10"><p>3.1.1 CONTROL: The AMS-02 project will use
JSC-25863A to implement the fracture control requirements of
NASA-STD-5003 and SSP-30558C. See attached table for fracture
classification of each structural element.</p>
<p>3.1.1 SVM: Compliance with the fracture control requirements of
NASA-STD-5003 and SSP-30558C will be verified by approval of fracture
control summary by JSC ES4/Materials and Processes Branch.</p>
<p>3.1.1 STATUS: Open</p></td>
<td colspan="2"></td>
</tr>
<tr class="odd">
<td colspan="10">4. CAUSE: Use of counterfeit, substandard or inadequate
fasteners.</td>
<td colspan="2"></td>
</tr>
<tr class="even">
<td colspan="10"><p>4.1 CONTROL: All fasteners, including safety
critical fasteners contained in components supplied by subcontractors,
#8 (~3 mm) and larger are selected and tested in accordance with JSC
23642E. Structural fasteners that are safety critical (structurally) are
selected to be size #8 or larger.</p>
<p>4.1.1 SVM: AMS-02 Chief Engineer will collect all Certification
documentation (including documentation for safety critical fasteners
contained in components supplied by subcontractors) to verify that all
structural fasteners will be #8 or larger and lot testing has been
performed by JSC personnel to verify compliance with strength and
chemical composition requirements of JSC-23642E. Chief Engineer’s Report
on Completion will close action.</p>
<p>4.1.1 STATUS: Open</p></td>
<td colspan="2"></td>
</tr>
<tr class="odd">
<td colspan="10"><p>4.2 CONTROL: All hardware that is capable of
releasing a mass of 0.25 lbs. or larger due to fastener(s) failure will
be attached with #8 or larger fasteners.</p>
<p>4.2.1 SVM: Review of design by AMS-02 Project to ensure
compliance.</p>
<p>4.2.2 SVM: Inspection of as built design.</p>
<p>4.2.1 STATUS: Open</p>
<p>4.2.2 STATUS: Open</p></td>
<td colspan="2"></td>
</tr>
<tr class="even">
<td colspan="10">5. CAUSE: Loosening of safety critical fasteners.</td>
<td colspan="2"></td>
</tr>
<tr class="odd">
<td colspan="10"><p>5.1 CONTROL: Safety-critical fasteners, including
safety critical fasteners contained in components supplied by
subcontractors, inadvertent back-off will be prevented by the use of
locking inserts/nuts, self-locking bolts, safety wire and fastener
preload/torque.</p>
<p>5.1.1 SVM: Certification documentation (including documentation for
safety critical fasteners contained in components supplied by
subcontractors) that appropriate back off prevention methods were
used.</p>
<p>5.1.1 STATUS: Open</p></td>
<td colspan="2"></td>
</tr>
<tr class="even">
<td colspan="10"><p>5.2 CONTROL: For applications where small fasteners
are used that utilized chemical thread lock (e.g. “Loctite”,
“Vibratite”) to prevent backout, fasteners will be contained within the
structure of the AMS-02 or its subelements. This controls the potential
release of mass while on the ISS truss.</p>
<p>5.2.1 SVM: Review of Design</p>
<p>5.2.1 STATUS: Open</p></td>
<td colspan="2"></td>
</tr>
<tr class="odd">
<td colspan="10"><p>5.3 CONTROL: In limited applications small fasteners
capable of being released and not contained by AMS-02 Structures or its
subelements and too small to utilize approved backout prevention
methodologies have implemented a potting/embedding of the fastener head
within an epoxy (type) compound to contain the fastener. This
implementation requires complete encapsulation of the fastener head (nut
where applicable) in a space qualified adhesive material.</p>
<p>5.3.1 SVM: Inspection of fastener potting/embedding. (Cumulative
report will close this verification.)</p>
<p>5.3.1 STATUS: Open</p></td>
<td colspan="2"></td>
</tr>
<tr class="even">
<td colspan="10">6. CAUSE: Loss of structural integrity of welds.</td>
<td colspan="2"></td>
</tr>
<tr class="odd">
<td colspan="10"><p>6.1 CONTROL: The welds will have positive margins of
safety during all mission phases, for the factors of safety specified in
Control 1.1.</p>
<p>6.1.1 SVM: Structural Analysis demonstrating positive margin of
safety</p>
<p>6.1.1 STATUS: Open</p></td>
<td colspan="2"></td>
</tr>
<tr class="even">
<td colspan="10"><p>6.2 CONTROL: Welding Processes are controlled by
implementation of the AMS-02 Weld Control Plans and Procedures.</p>
<p>6.2.1 SVM: Review and approval of He Tank Weld Control Plan by
ES4/Materials and Processes Branch.</p>
<p>6.2.2 SVM: Review and approval of the Vacuum Case Welding Plan by
ES4/Materials and Processes Branch</p>
<p>6.2.3 SVM: Welds will be inspected: Dye Penetrant, X-ray, and/or
Ultrasound</p>
<p>6.2.1 STATUS: Closed. Confirmation of ES4 acceptance of Weld Plan
Review by ESCG/D. Rybiki and ES4/G. Ecord transmitted by email from
ES4/B. S. Files on November 20, 2006 to AMS-02 Chief Engineer Chris
Tutt</p>
<p>6.2.2 STATUS: Closed. Confirmation of ES4 acceptance of Weld Plan
Review by ESCG/D. Rybiki and ES4/G. Ecord transmitted by email from
ES4/B. S. Files on November 20, 2006 to AMS-02 Chief Engineer Chris
Tutt</p>
<p>6.2.3 STATUS: Open</p></td>
<td colspan="2"></td>
</tr>
<tr class="odd">
<td colspan="10">7. CAUSE: Improper manufacture and/ or assembly.</td>
<td colspan="2"></td>
</tr>
<tr class="even">
<td colspan="10"><p>7.1 CONTROL: Approved drawings and procedures,
including tool control, will be used for manufacturing and assembly.</p>
<p>7.1.1 SVM: Certification documentation will be provided to verify
proper manufacturing/assembly of AMS-02 hardware (including all
composite materials).</p>
<p>7.1.1 STATUS: Open</p></td>
<td colspan="2"></td>
</tr>
<tr class="odd">
<td colspan="10">8. CAUSE: Improper preload or creeping of the
Cryomagnet support system straps.</td>
<td colspan="2"></td>
</tr>
<tr class="even">
<td colspan="10"><p>8.1 CONTROL: Cryomagnet support system straps will
be preloaded prior to flight to provide a balanced support load for the
Cryomagnet. Preload is established by compressing a Belleville washer
stack on a freestanding jig prior to installation. Preload strain
measurements are made in conjunction with the initial setup.</p>
<p>8.1.1 SVM: Verify preload at time of installation (MIP)</p>
<p>8.1.2 SVM: Long term creep analysis to ensure that the Cryomagnet
support system straps will not be out of tolerance for any flight regime
or over the life of the payload.</p>
<p>8.1.1 STATUS: Open</p>
<p>8.1.2 STATUS: Closed. Jacobs Memorandum ESCG-4039-05-SP-DO-0003 dated
4 July, 2005</p></td>
<td colspan="2"></td>
</tr>
<tr class="odd">
<td colspan="10">9. CAUSE: Damage to composite structural components
during manufacturing, assembly operations, ground handling, and/or
ground transportation.</td>
<td colspan="2"></td>
</tr>
<tr class="even">
<td colspan="10"><p>9.1 CONTROL: Each supplier/developer of composite
structures will provide special handling procedures and requirements
which are developed into work instructions for manufacturing, assembly
operations, ground handling and/or ground transportation. Quality
assurance representatives oversee the implementation of these work
instructions to protect the composite structures.</p>
<p>9.1.1 SVM: QA review of procedures and certification of procedure
completion.</p>
<p>9.1.1 STATUS: Open</p></td>
<td colspan="2"></td>
</tr>
<tr class="odd">
<td colspan="10">10. CAUSE: Degradation of composite structural
components by atomic oxygen.</td>
<td colspan="2"></td>
</tr>
<tr class="even">
<td colspan="10"><p>10.1 CONTROL: All composite structures are covered
with thermal blankets, structures and/or coatings to assure non-metallic
components are not in a direct line of sight of atomic oxygen.</p>
<p>10.1.1 SVM: Review of design.</p>
<p>10.1.2 SVM: Inspection of as built hardware.</p>
<p>10.1.1 STATUS: Closed. Design of all load bearing composite
structures indicate no line of sight to atomic oxygen. Memorandum
ESCG-4390-06-SP-MEMO-0005, “Composite Structural Elements,” dated 13
March 2006, AMS-02 Chief Engineer Chris Tutt.</p>
<p>10.1.2 STATUS: Open</p></td>
<td colspan="2"></td>
</tr>
<tr class="odd">
<td colspan="10">11. CAUSE: Improper Preload of PAS</td>
<td colspan="2"></td>
</tr>
<tr class="even">
<td colspan="10"><p>11.1 CONTROL: In order to establish the proper
stiffness and preload of the AMS-02 when grappled by the ISS active PAS
the AMS-02 is designed to have an adjustable configuration on the AMS-02
PAS element. The stiffness has been established to meet the requirement
of SSP 57003.</p>
<p>11.1.1 SVM: Structural Analysis (for Stiffness)</p>
<p>11.1.2 SVM: Interface testing on S3 Truss with AMS-02 Flight PAS.</p>
<p>11.1.3 SVM: Inspection of Flight hardware to confirm proper
configuration of adjustment prior to flight.</p>
<p>11.1.1 STATUS: Closed. Jacobs Sverdrup Memo
ESCG-4390-06-SP-MEMO-0001, “Mechanical Design of the Payload Attach
System (PAS)”, Dated 8 January, 2006 from AMS-02 Chief Engineer.</p>
<p>11.1.2 STATUS: Closed. Memo ESCG-4390-05-SP-MEMO-0012, “Functional
Testing of the Payload Attach System” dated 28 December 2005, from
AMS-02 Chief Engineer Chris Tutt.</p>
<p>11.1.3 STATUS: Open</p></td>
<td colspan="2"></td>
</tr>
<tr class="odd">
<td colspan="10">12. CAUSE: Reconfiguration of Mechanical
Components</td>
<td colspan="2"></td>
</tr>
<tr class="even">
<td colspan="10"><p>12.1 CONTROL: The EVA release of the PAS mechanism
is structurally capable of enduring Orbiter return loads with a positive
margin of safety regardless of return configuration (fully reinstalled
with preload release screws returned to hardstop configuration or
disengaged). Operation of this mechanism is contingency response only to
failure of ISS Payload Attach Site Mechanism.</p>
<p>12.1.1 SVM: Structural Analysis</p>
<p>12.1.1 STATUS: Open</p></td>
<td colspan="2"></td>
</tr>
<tr class="odd">
<td colspan="10"><p>12.2 CONTROL: The EVA reconfigurable ROEU Interface
support bracket hinge will be capable of supporting Orbiter return loads
with a positive margin of safety even if only one of the two EVA
operated pip pins are installed. Nominal procedures will install two
pins. Operation of this mechanism is contingency only in response to an
envelope clearance request from the ISS.</p>
<p>12.2.1 SVM: Structural Analysis</p>
<p>12.2.1 STATUS: Open</p></td>
<td colspan="2"></td>
</tr>
<tr class="even">
<td colspan="10">Notes:</td>
<td colspan="2"></td>
</tr>
</tbody>
</table>

  -----------------------------------------------------------------------
  ACRONYMS                           
  ---------------------------------- ------------------------------------
  1-D -- one dimensional             lbf -- pounds force

  ACC -- Anticoincidence Counter     lbs -- Pounds

  AIAA -- American Institute of      LMSEAT -- Lockheed Martin Science
  Aeronautics and Astronautics       Engineering and Test Contract

  AIDC -- Aerospace Industrial       LT -- Lower Time of Flight
  Development Corporation (Taiwan)   

  Al - Aluminum                      LTOF -- Lower Time of Flight

  AMICA - Astro Mapper for           MUA -- Material Usage Agreement
  Instruments Check of Attitude      

  AMS-02 -- Alpha Magnetic           MIT -- Massachusetts Institute of
  Spectrometer 02                    Technology

  ANSI- American National Standards  mm -- Millimeter
  Institute                          

  ARDE -- Company Name, Arde' Inc.   NDE -- Non-Destructive Examination

  ASR -- AMS-02 Support Rods         PAS -- Payload Attach Site (ISS
                                     Component, e.g. Active PAS)

  ASTM -- American Society for       PAS -- Payload Attach System (AMS-02
  Testing and Materials              component)

  ASTS -- AMS Star Tracker Support   PCB -- Printed Circuit Board
  Structure                          

  ATR -- AMS-02 Tracker Rods         PMT -- Photomultiplier Tube

  CERN - *Conseil Européen pour la   Ops - Operations
  Recherche Nucléaire* (European     
  Council for Nuclear Research)      

  CFRP -- Carbon Fiber Reinforced    QA -- Quality Assurance
  Panel                              

  C of C -- Certificate of           RAV --
  Compliance                         

  Comp -- Compressive                RICH -- Ring Imaging Cherenkov
                                     Counter

  CMA -- Contract Management and     ROEU -- Remotely Operated Electrical
  Administration                     Umbilical

  CO2 -- CO~2~, Carbon Dioxide       RT -- Race track

  CRISA - Computadores, Redes e      RTEF -- Race track End Frame
  Ingeniería, S.A (Division of EADS  
  Astrium)                           

  CSIST -- Chung-shan Institute of   RWTH -- Rheinisch-Westfälische
  Science and Technology             Technische Hochschule
                                     (Rhenish-Westphalian Technical
                                     University)

  DCLA -- Design Coupled Loads       SCL -- Space Cryomagnetics
  Analysis                           Laboratory (also known as Scientific
                                     Magnetics)

  Deg - Degrees                      SFHe -- Superfluid Helium

  EADS -- European Aeronautics       Si -- Silicon
  Defense and Space Company          

  ECAL -- Electromagnetic            STA -- Structural Test Article
  Calorimeter                        

  E-Crate -- Electronics Crate       SVM -- Safety Verification Method

  EVA -- Extravehicular Activity     SVP -- Structural Verification Plan

  FEM -- Finite Element Method       TCS -- Thermal Control System

  FOS -- Factor of Safety            TOF -- Time of Flight

  FS -- Factor of Safety             TRD -- Transition Radiation Detector

  He -- Helium                       ult -- Ultimate

  HV -- High Voltage                 UPS -- Uninterruptible Power Supply

  Hz -- Hertz                        USS -- Unique Support Structure

  I/F -- Interface                   UT -- Upper Time of Flight

  in -- inch                         UTOF -- Upper Time of Flight

  INFN - *Istituto Nazionale di      VC -- Vacuum Case
  Fisica Nucleare*                   

  ISATEC -- Company Name             VCM -- Volatile Condensable Material

  ksi -- thousand pounds per square  Xe -- Xenon
  inch                               

  L -- Launch                        XPD -- Generic Power Distribution
                                     Box (First letter changed to
                                     designate specific subsystem)
  -----------------------------------------------------------------------

**AMS-02 Structural Margin Tables**

+----------+------+---+----------+------+---+-----+-----+-----------------+
| **Margin |      |   |          |      |   |     |     |                 |
| of       |      |   |          |      |   |     |     |                 |
| Safety   |      |   |          |      |   |     |     |                 |
| Summary  |      |   |          |      |   |     |     |                 |
| for      |      |   |          |      |   |     |     |                 |
| Tr       |      |   |          |      |   |     |     |                 |
| ansition |      |   |          |      |   |     |     |                 |
| R        |      |   |          |      |   |     |     |                 |
| adiation |      |   |          |      |   |     |     |                 |
| Detector |      |   |          |      |   |     |     |                 |
| (TRD)    |      |   |          |      |   |     |     |                 |
| Str      |      |   |          |      |   |     |     |                 |
| ucture** |      |   |          |      |   |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| Item     | Dra  | M |          | Mate |   | M   | Mar | Comments        |
|          | wing | a |          | rial |   | ax. | gin |                 |
|          | nu   | t |          | a    |   | a   | of  |                 |
|          | mber | e |          | llow |   | ppl | Saf |                 |
|          |      | r |          | able |   | ied | ety |                 |
|          |      | i |          | st   |   | str | (u  |                 |
|          |      | a |          | ress |   | ess | lt) |                 |
|          |      | l |          | (    |   | (k  | FS= |                 |
|          |      | a |          | ksi) |   | si) | 2.0 |                 |
|          |      | n |          |      |   |     |     |                 |
|          |      | d |          |      |   |     |     |                 |
|          |      | t |          |      |   |     |     |                 |
|          |      | e |          |      |   |     |     |                 |
|          |      | m |          |      |   |     |     |                 |
|          |      | p |          |      |   |     |     |                 |
|          |      | e |          |      |   |     |     |                 |
|          |      | r |          |      |   |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| TRD      |      |   |          |      |   |     |     |                 |
| Support  |      |   |          |      |   |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| M        |  181 | 7 |          | 62   |   | 1   | 1   | Page 31 Note 1  |
| s        | 1/60 | 0 |          |      |   | 5.4 | .02 |                 |
| tructure | 0002 | 7 |          |      |   |     |     |                 |
|          | 1 V1 | 5 |          |      |   |     |     |                 |
|          |      | - |          |      |   |     |     |                 |
|          |      | T |          |      |   |     |     |                 |
|          |      | 7 |          |      |   |     |     |                 |
|          |      | 3 |          |      |   |     |     |                 |
|          |      | 5 |          |      |   |     |     |                 |
|          |      | 1 |          |      |   |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| Corner   | 181  | 7 |          | 57   |   | 2   | 0   | Page 12, Note   |
| brackets | 1/60 | 0 |          |      |   | 2.9 | .24 | 30              |
|          | 0001 | 7 |          |      |   |     |     |                 |
|          | V1   | 5 |          |      |   |     |     |                 |
|          |      | - |          |      |   |     |     |                 |
|          |      | T |          |      |   |     |     |                 |
|          |      | 7 |          |      |   |     |     |                 |
|          |      | 3 |          |      |   |     |     |                 |
|          |      | 5 |          |      |   |     |     |                 |
|          |      | 1 |          |      |   |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| Upper    | 181  | 7 |          | 60   |   | 2   | 0   | Page 14, Note   |
| bracket  | 1/60 | 0 |          |      |   | 2.8 | .32 | 30              |
| right    | _000 | 7 |          |      |   |     |     |                 |
|          | 3-01 | 5 |          |      |   |     |     |                 |
|          | _V1  | - |          |      |   |     |     |                 |
|          |      | T |          |      |   |     |     |                 |
|          |      | 7 |          |      |   |     |     |                 |
|          |      | 3 |          |      |   |     |     |                 |
|          |      | 5 |          |      |   |     |     |                 |
|          |      | 1 |          |      |   |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| Upper    | 181  | 7 |          | 60   |   | 2   | 0   | Page 14, Note   |
| bracket  | 1/60 | 0 |          |      |   | 2.8 | .32 | 30              |
| left     | _000 | 7 |          |      |   |     |     |                 |
|          | 4-01 | 5 |          |      |   |     |     |                 |
|          | _V1  | - |          |      |   |     |     |                 |
|          |      | T |          |      |   |     |     |                 |
|          |      | 7 |          |      |   |     |     |                 |
|          |      | 3 |          |      |   |     |     |                 |
|          |      | 5 |          |      |   |     |     |                 |
|          |      | 1 |          |      |   |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| TRD      |      |   |          |      |   |     |     |                 |
| Octagon  |      |   |          |      |   |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| Octagon  | am   | C |          | 145  |   | 7   | 0.  | Page 20, Note   |
| panels   | s191 | a |          |      |   | 2.3 | 002 | 30              |
|          | 2i-3 | r |          |      |   |     |     |                 |
|          | d-02 | b |          |      |   |     |     |                 |
|          | ams1 | o |          |      |   |     |     |                 |
|          | 912p | n |          |      |   |     |     |                 |
|          |      | f |          |      |   |     |     |                 |
|          |      | i |          |      |   |     |     |                 |
|          |      | b |          |      |   |     |     |                 |
|          |      | e |          |      |   |     |     |                 |
|          |      | r |          |      |   |     |     |                 |
|          |      | s |          |      |   |     |     |                 |
|          |      | k |          |      |   |     |     |                 |
|          |      | i |          |      |   |     |     |                 |
|          |      | n |          |      |   |     |     |                 |
|          |      |   |          |      |   |     |     |                 |
|          |      | A |          |      |   |     |     |                 |
|          |      | l |          |      |   |     |     |                 |
|          |      | . |          |      |   |     |     |                 |
|          |      | 5 |          |      |   |     |     |                 |
|          |      | 0 |          |      |   |     |     |                 |
|          |      | 5 |          |      |   |     |     |                 |
|          |      | 6 |          |      |   |     |     |                 |
|          |      | c |          |      |   |     |     |                 |
|          |      | o |          |      |   |     |     |                 |
|          |      | r |          |      |   |     |     |                 |
|          |      | e |          |      |   |     |     |                 |
|          |      | 1 |          |      |   |     |     |                 |
|          |      | / |          |      |   |     |     |                 |
|          |      | 8 |          |      |   |     |     |                 |
|          |      | i |          |      |   |     |     |                 |
|          |      | n |          |      |   |     |     |                 |
|          |      | c |          |      |   |     |     |                 |
|          |      | e |          |      |   |     |     |                 |
|          |      | l |          |      |   |     |     |                 |
|          |      | l |          |      |   |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| Octagon  | ams  | C |          | 145  |   | 4   | 0   | Page 24, Note 1 |
| panel    | 02   | a |          |      |   | 3.7 | .66 |                 |
| flanges  | 1    | r |          |      |   |     |     |                 |
|          | 912p | b |          |      |   |     |     |                 |
|          | De   | o |          |      |   |     |     |                 |
|          | tail | n |          |      |   |     |     |                 |
|          | U,V  | f |          |      |   |     |     |                 |
|          |      | i |          |      |   |     |     |                 |
|          |      | b |          |      |   |     |     |                 |
|          |      | e |          |      |   |     |     |                 |
|          |      | r |          |      |   |     |     |                 |
|          |      | s |          |      |   |     |     |                 |
|          |      | k |          |      |   |     |     |                 |
|          |      | i |          |      |   |     |     |                 |
|          |      | n |          |      |   |     |     |                 |
|          |      |   |          |      |   |     |     |                 |
|          |      | A |          |      |   |     |     |                 |
|          |      | l |          |      |   |     |     |                 |
|          |      | . |          |      |   |     |     |                 |
|          |      | 5 |          |      |   |     |     |                 |
|          |      | 0 |          |      |   |     |     |                 |
|          |      | 5 |          |      |   |     |     |                 |
|          |      | 6 |          |      |   |     |     |                 |
|          |      | c |          |      |   |     |     |                 |
|          |      | o |          |      |   |     |     |                 |
|          |      | r |          |      |   |     |     |                 |
|          |      | e |          |      |   |     |     |                 |
|          |      | 1 |          |      |   |     |     |                 |
|          |      | / |          |      |   |     |     |                 |
|          |      | 8 |          |      |   |     |     |                 |
|          |      | i |          |      |   |     |     |                 |
|          |      | n |          |      |   |     |     |                 |
|          |      | c |          |      |   |     |     |                 |
|          |      | e |          |      |   |     |     |                 |
|          |      | l |          |      |   |     |     |                 |
|          |      | l |          |      |   |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| Upper    | ams  | T |          | 116  |   | -2  | 1   | Page 25, Note 1 |
| flange   | 02   | 3 |          |      |   | 7.7 | .10 |                 |
| reinf    | 1996 | 3 |          |      |   |     |     |                 |
| orcement | f    | T |          |      |   |     |     |                 |
| ring     |      | e |          |      |   |     |     |                 |
|          |      | n |          |      |   |     |     |                 |
|          |      | a |          |      |   |     |     |                 |
|          |      | x |          |      |   |     |     |                 |
|          |      | F |          |      |   |     |     |                 |
|          |      | a |          |      |   |     |     |                 |
|          |      | b |          |      |   |     |     |                 |
|          |      | r |          |      |   |     |     |                 |
|          |      | i |          |      |   |     |     |                 |
|          |      | c |          |      |   |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| Upper    | ams  | C |          | 116  |   | -3  | 0   | Page 27, Note 1 |
| cover    | 02   | a |          |      |   | 2.2 | .80 |                 |
|          | 1    | r |          |      |   |     |     |                 |
|          | 942g | b |          |      |   |     |     |                 |
|          |      | o |          |      |   |     |     |                 |
|          |      | n |          |      |   |     |     |                 |
|          |      | f |          |      |   |     |     |                 |
|          |      | i |          |      |   |     |     |                 |
|          |      | b |          |      |   |     |     |                 |
|          |      | e |          |      |   |     |     |                 |
|          |      | r |          |      |   |     |     |                 |
|          |      | s |          |      |   |     |     |                 |
|          |      | k |          |      |   |     |     |                 |
|          |      | i |          |      |   |     |     |                 |
|          |      | n |          |      |   |     |     |                 |
|          |      |   |          |      |   |     |     |                 |
|          |      | A |          |      |   |     |     |                 |
|          |      | l |          |      |   |     |     |                 |
|          |      | . |          |      |   |     |     |                 |
|          |      | 5 |          |      |   |     |     |                 |
|          |      | 0 |          |      |   |     |     |                 |
|          |      | 5 |          |      |   |     |     |                 |
|          |      | 6 |          |      |   |     |     |                 |
|          |      | 3 |          |      |   |     |     |                 |
|          |      | / |          |      |   |     |     |                 |
|          |      | 1 |          |      |   |     |     |                 |
|          |      | 6 |          |      |   |     |     |                 |
|          |      | c |          |      |   |     |     |                 |
|          |      | e |          |      |   |     |     |                 |
|          |      | l |          |      |   |     |     |                 |
|          |      | l |          |      |   |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| **Margin |      |   |          |      |   |     |     |                 |
| of       |      |   |          |      |   |     |     |                 |
| Safety   |      |   |          |      |   |     |     |                 |
| Summary  |      |   |          |      |   |     |     |                 |
| for      |      |   |          |      |   |     |     |                 |
| Tr       |      |   |          |      |   |     |     |                 |
| ansition |      |   |          |      |   |     |     |                 |
| R        |      |   |          |      |   |     |     |                 |
| adiation |      |   |          |      |   |     |     |                 |
| Detector |      |   |          |      |   |     |     |                 |
| (TRD)    |      |   |          |      |   |     |     |                 |
| Gas      |      |   |          |      |   |     |     |                 |
| System   |      |   |          |      |   |     |     |                 |
| Str      |      |   |          |      |   |     |     |                 |
| ucture** |      |   |          |      |   |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| Item     | Dra  | M |          | Mate |   | M   | Mar | Comments        |
|          | wing | a |          | rial |   | ax. | gin |                 |
|          | nu   | t |          | a    |   | a   | of  |                 |
|          | mber | e |          | llow |   | ppl | Saf |                 |
|          |      | r |          | able |   | ied | ety |                 |
|          |      | i |          | st   |   | str | (u  |                 |
|          |      | a |          | ress |   | ess | lt) |                 |
|          |      | l |          | (    |   | (k  | FS= |                 |
|          |      | a |          | ksi) |   | si) | 2.0 |                 |
|          |      | n |          |      |   |     |     |                 |
|          |      | d |          |      |   |     |     |                 |
|          |      | t |          |      |   |     |     |                 |
|          |      | e |          |      |   |     |     |                 |
|          |      | m |          |      |   |     |     |                 |
|          |      | p |          |      |   |     |     |                 |
|          |      | e |          |      |   |     |     |                 |
|          |      | r |          |      |   |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| Box S    |      | 7 |          | 66.1 |   | 3   | 0   | Page 21, Note 2 |
| plate    |      | 0 |          |      |   | 0.6 | .08 |                 |
|          |      | 5 |          |      |   |     |     |                 |
|          |      | 0 |          |      |   |     |     |                 |
|          |      | - |          |      |   |     |     |                 |
|          |      | T |          |      |   |     |     |                 |
|          |      | 7 |          |      |   |     |     |                 |
|          |      | 4 |          |      |   |     |     |                 |
|          |      | 5 |          |      |   |     |     |                 |
|          |      | 1 |          |      |   |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| Xe tank  |      | 6 |          | 42   |   | 4.6 | 1.4 | Page 21 Note 2  |
| bracket  |      | 0 |          |      |   |     |     |                 |
|          |      | 6 |          |      |   |     |     |                 |
|          |      | 1 |          |      |   |     |     |                 |
|          |      | - |          |      |   |     |     |                 |
|          |      | T |          |      |   |     |     |                 |
|          |      | 6 |          |      |   |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| Lower    |      | 7 |          | 66.1 |   | 1   | 1   | Page 21, Note 2 |
| bracket  |      | 0 |          |      |   | 2.3 | .69 |                 |
|          |      | 5 |          |      |   |     |     |                 |
|          |      | 0 |          |      |   |     |     |                 |
|          |      | - |          |      |   |     |     |                 |
|          |      | T |          |      |   |     |     |                 |
|          |      | 7 |          |      |   |     |     |                 |
|          |      | 4 |          |      |   |     |     |                 |
|          |      | 5 |          |      |   |     |     |                 |
|          |      | 1 |          |      |   |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| Box C    |      | 6 |          | 49.3 |   | 2   | 0   | Page 15 Note 3  |
| base     |      | 0 |          |      |   | 0.3 | .21 |                 |
| plate    |      | 6 |          |      |   |     |     |                 |
|          |      | 1 |          |      |   |     |     |                 |
|          |      | - |          |      |   |     |     |                 |
|          |      | T |          |      |   |     |     |                 |
|          |      | 6 |          |      |   |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| Valve    |      | 6 |          | 49.3 |   | 1   | 0   | Page 15 Note 3  |
| bracket  |      | 0 |          |      |   | 3.2 | .86 |                 |
|          |      | 6 |          |      |   |     |     |                 |
|          |      | 1 |          |      |   |     |     |                 |
|          |      | - |          |      |   |     |     |                 |
|          |      | T |          |      |   |     |     |                 |
|          |      | 6 |          |      |   |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| **Margin |      |   |          |      |   |     |     |                 |
| of       |      |   |          |      |   |     |     |                 |
| Safety   |      |   |          |      |   |     |     |                 |
| Summary  |      |   |          |      |   |     |     |                 |
| of       |      |   |          |      |   |     |     |                 |
| AMS-02   |      |   |          |      |   |     |     |                 |
| Upper    |      |   |          |      |   |     |     |                 |
| Time of  |      |   |          |      |   |     |     |                 |
| Flight   |      |   |          |      |   |     |     |                 |
| (UTOF)** |      |   |          |      |   |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| Item     | Dra  | M |          | Mate |   | M   | Mar | Comments        |
|          | wing | a |          | rial |   | ax. | gin |                 |
|          | nu   | t |          | a    |   | a   | of  |                 |
|          | mber | e |          | llow |   | ppl | Saf |                 |
|          |      | r |          | able |   | ied | ety |                 |
|          |      | i |          | st   |   | str | (u  |                 |
|          |      | a |          | ress |   | ess | lt) |                 |
|          |      | l |          | (    |   | (k  | FS= |                 |
|          |      | a |          | ksi) |   | si) | 2.0 |                 |
|          |      | n |          |      |   |     |     |                 |
|          |      | d |          |      |   |     |     |                 |
|          |      | t |          |      |   |     |     |                 |
|          |      | e |          |      |   |     |     |                 |
|          |      | m |          |      |   |     |     |                 |
|          |      | p |          |      |   |     |     |                 |
|          |      | e |          |      |   |     |     |                 |
|          |      | r |          |      |   |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| Upper    | ams  | 7 |          | 64   |   | 3   | 0   | Page 57, Note 4 |
| brackets | TOF  | 0 |          |      |   | 1.4 | .02 |                 |
|          | 0    | 7 |          |      |   |     |     |                 |
|          | 8-01 | 5 |          |      |   |     |     |                 |
|          | -006 | - |          |      |   |     |     |                 |
|          | UT   | T |          |      |   |     |     |                 |
|          |      | 7 |          |      |   |     |     |                 |
|          |      | 3 |          |      |   |     |     |                 |
|          |      | 5 |          |      |   |     |     |                 |
|          |      | 1 |          |      |   |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| Lower    | ams  | 7 |          | 64   |   | 1   | 0   | Page 57, Note 4 |
| brackets | TOF  | 0 |          |      |   | 6.1 | .98 |                 |
|          | 0    | 7 |          |      |   |     |     |                 |
|          | 8-01 | 5 |          |      |   |     |     |                 |
|          | -001 | - |          |      |   |     |     |                 |
|          | UT   | T |          |      |   |     |     |                 |
|          |      | 7 |          |      |   |     |     |                 |
|          |      | 3 |          |      |   |     |     |                 |
|          |      | 5 |          |      |   |     |     |                 |
|          |      | 1 |          |      |   |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| Ex       | ams  | 7 |          | 64   |   | 1   | 0   | Page 57, Note 4 |
| tensions | TOF  | 0 |          |      |   | 6.1 | .98 |                 |
|          | 0    | 7 |          |      |   |     |     |                 |
|          | 8-01 | 5 |          |      |   |     |     |                 |
|          | -008 | - |          |      |   |     |     |                 |
|          | UT   | T |          |      |   |     |     |                 |
|          |      | 7 |          |      |   |     |     |                 |
|          |      | 3 |          |      |   |     |     |                 |
|          |      | 5 |          |      |   |     |     |                 |
|          |      | 1 |          |      |   |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| H        | ams  | 2 |          | 62.9 |   | 1   | 0   | Page 57, Note 4 |
| oneycomb | TOF  | 0 |          |      |   | 8.3 | .72 |                 |
| skins    | 0    | 2 |          |      |   |     |     |                 |
|          | 8-02 | 4 |          |      |   |     |     |                 |
|          | -002 | - |          |      |   |     |     |                 |
|          | UT   | T |          |      |   |     |     |                 |
|          |      | 8 |          |      |   |     |     |                 |
|          |      | 1 |          |      |   |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| S        | ams  | 7 |          | 64   |   | 8   | 2   | Page 57, Note 4 |
| econdary | TOF  | 0 |          |      |   | .1  | .92 |                 |
| Brackets | 0    | 7 |          |      |   |     |     |                 |
|          | 2-01 | 5 |          |      |   |     |     |                 |
|          | -005 | - |          |      |   |     |     |                 |
|          | UT   | T |          |      |   |     |     |                 |
|          |      | 7 |          |      |   |     |     |                 |
|          |      | 3 |          |      |   |     |     |                 |
|          |      | 5 |          |      |   |     |     |                 |
|          |      | 1 |          |      |   |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| Sensor   | ams  | C |          | X =  |   | X=  | 0   | Page 58, Note   |
| Boxes    | TOF  | F |          | 1    |   | 4.9 | .51 | 4, Margin of    |
|          | 09   | R |          | 15.9 |   |     |     | safety          |
|          | -001 | P |          |      |   | Y=  |     |                 |
|          | UT   | T |          | Y =  |   | 7.4 |     | Note 5          |
|          |      | 3 |          | 1    |   |     |     |                 |
|          |      | 0 |          | 15.9 |   | XY= |     |                 |
|          |      | 0 |          |      |   | 4.6 |     |                 |
|          |      | f |          | XY   |   |     |     |                 |
|          |      | a |          | =    |   |     |     |                 |
|          |      | b |          | 14.3 |   |     |     |                 |
|          |      | r |          |      |   |     |     |                 |
|          |      | i |          |      |   |     |     |                 |
|          |      | c |          |      |   |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| Scin     |      | C |          | X =  |   | X=2 | 0   | Page 58, Note   |
| tillator |      | F |          | 1    |   | 2.2 | .11 | 4, Margin of    |
| Supports |      | R |          | 15.9 |   |     |     | safety          |
|          |      | P |          |      |   | Y=2 |     |                 |
|          |      | T |          | Y    |   | 5.7 |     | Note 5          |
|          |      | 3 |          | =1   |   |     |     |                 |
|          |      | 0 |          | 15.9 |   | XY= |     |                 |
|          |      | 0 |          |      |   | 3.8 |     |                 |
|          |      | f |          | XY=  |   |     |     |                 |
|          |      | a |          | 14.3 |   |     |     |                 |
|          |      | b |          |      |   |     |     |                 |
|          |      | r |          |      |   |     |     |                 |
|          |      | i |          |      |   |     |     |                 |
|          |      | c |          |      |   |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| PMT      | ams  | C |          | X    |   | X=1 | 1   | Page 58, Note   |
| Boxes    | TOF  | F |          | =1   |   | 0.4 | .70 | 4, Margin of    |
| supports | 0    | R |          | 15.9 |   |     |     | safety          |
|          | 5-05 | P |          |      |   | Y=9 |     |                 |
|          | -001 | T |          | Y    |   | .75 |     | Note 5          |
|          | UT   | 3 |          | =1   |   |     |     |                 |
|          |      | 0 |          | 15.9 |   | XY= |     |                 |
|          |      | 0 |          |      |   | 2.4 |     |                 |
|          |      | f |          | XY = |   |     |     |                 |
|          |      | a |          | 14.3 |   |     |     |                 |
|          |      | b |          |      |   |     |     |                 |
|          |      | r |          |      |   |     |     |                 |
|          |      | i |          |      |   |     |     |                 |
|          |      | c |          |      |   |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| **Margin |      |   |          |      |   |     |     |                 |
| of       |      |   |          |      |   |     |     |                 |
| Safety   |      |   |          |      |   |     |     |                 |
| Summary  |      |   |          |      |   |     |     |                 |
| of       |      |   |          |      |   |     |     |                 |
| AMS-02   |      |   |          |      |   |     |     |                 |
| Lower    |      |   |          |      |   |     |     |                 |
| Time of  |      |   |          |      |   |     |     |                 |
| Flight   |      |   |          |      |   |     |     |                 |
| (LTOF)** |      |   |          |      |   |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| Item     | Dra  |   | Material | Mate |   | M   | Mar | Comments        |
|          | wing |   | and      | rial |   | ax. | gin |                 |
|          | nu   |   | temper   | a    |   | a   | of  |                 |
|          | mber |   |          | llow |   | ppl | Saf |                 |
|          |      |   |          | able |   | ied | ety |                 |
|          |      |   |          | st   |   | str | (u  |                 |
|          |      |   |          | ress |   | ess | lt) |                 |
|          |      |   |          | (    |   | (k  | FS= |                 |
|          |      |   |          | ksi) |   | si) | 2.0 |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| Beam A   | ams  |   | 70       | 64   |   | 3   | 0   | Page 76, Note 6 |
|          | TOF  |   | 75-T7351 |      |   | 0.6 | .05 |                 |
|          | 0    |   |          |      |   |     |     |                 |
|          | 4-01 |   |          |      |   |     |     |                 |
|          | -001 |   |          |      |   |     |     |                 |
|          | LT   |   |          |      |   |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| Beam B   | ams  |   | 70       | 64   |   | 2   | 0   | Page 76, Note 6 |
|          | TOF  |   | 75-T7351 |      |   | 9.8 | .07 |                 |
|          | 0    |   |          |      |   |     |     |                 |
|          | 4-01 |   |          |      |   |     |     |                 |
|          | -002 |   |          |      |   |     |     |                 |
|          | LT   |   |          |      |   |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| Corner   | ams  |   | 70       | 64   |   | 1   | 1.9 | Page 76, Note 6 |
| beam     | TOF  |   | 75-T7351 |      |   | 1.0 |     |                 |
|          | 0    |   |          |      |   |     |     |                 |
|          | 4-01 |   |          |      |   |     |     |                 |
|          | -003 |   |          |      |   |     |     |                 |
|          | LT   |   |          |      |   |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| Upper    | ams  |   | 70       | 64   |   | 1   | 1   | Page 76, Note 6 |
| bracket  | TOF  |   | 75-T7351 |      |   | 0.7 | .98 |                 |
|          | 0    |   |          |      |   |     |     |                 |
|          | 4-01 |   |          |      |   |     |     |                 |
|          | -021 |   |          |      |   |     |     |                 |
|          | LT   |   |          |      |   |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| Lower    | ams  |   | 70       | 64   |   | 1   | \>  | Page 76, Note 6 |
| bracket  | TOF  |   | 75-T7351 |      |   | 0.0 | 2.0 |                 |
|          | 0    |   |          |      |   |     |     |                 |
|          | 4-01 |   |          |      |   |     |     |                 |
|          | -020 |   |          |      |   |     |     |                 |
|          | LT   |   |          |      |   |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| Internal | ams  |   | 70       | 64   |   | 13  | 1.4 | Page 76, Note 6 |
| bracket  | TOF  |   | 75-T7351 |      |   | .30 |     |                 |
|          | 0    |   |          |      |   |     |     |                 |
|          | 4-01 |   |          |      |   |     |     |                 |
|          | -018 |   |          |      |   |     |     |                 |
|          | LT   |   |          |      |   |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| Struts   | ams  |   | 70       | 64   |   | 14  | 1   | Page 76, Note 6 |
|          | TOF  |   | 75-T7351 |      |   | .60 | .18 |                 |
|          | 04-0 |   |          |      |   |     |     |                 |
|          | 1-01 |   |          |      |   |     |     |                 |
|          | -001 |   |          |      |   |     |     |                 |
|          | LT   |   |          |      |   |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| Sensor   | ams  |   | 70       | 64   |   | 17  | 0   | Page 76, Note 6 |
| Boxes    | TOF  |   | 75-T7351 |      |   | .84 | .79 |                 |
| Bracket  | 0    |   |          |      |   |     |     |                 |
|          | 4-01 |   |          |      |   |     |     |                 |
|          | -008 |   |          |      |   |     |     |                 |
|          | LT   |   |          |      |   |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| Sensor   | ams  |   | CFRP     | X =  |   | X=- | 1   | Page 77, Note 6 |
| Boxes    | TOF  |   | T300     | 1    |   | 9.7 | .56 | Margin of       |
|          | 02   |   | Fabric   | 15.9 |   | Y=  |     | safety          |
|          | -001 |   |          |      |   | 9.8 |     |                 |
|          | LT   |   |          | Y =  |   | XY= |     | Note 7          |
|          |      |   |          | 1    |   | 3.9 |     |                 |
|          |      |   |          | 15.9 |   |     |     |                 |
|          |      |   |          |      |   |     |     |                 |
|          |      |   |          | XY = |   |     |     |                 |
|          |      |   |          | 14.3 |   |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| B        | ams  |   | CFRP     | X =  |   | X=1 | 1   | Page 77, Note 6 |
| oxes/PMT | TOF  |   | T300     | 1    |   | 3.9 | .17 | Margin of       |
| Support  | 0    |   | Fabric   | 15.9 |   |     |     | safety          |
|          | 5-05 |   |          |      |   | Y   |     |                 |
|          | -001 |   |          | Y =  |   | =-1 |     | Note 7          |
|          | LT   |   |          | 1    |   | 7.4 |     |                 |
|          |      |   |          | 15.9 |   | X   |     |                 |
|          |      |   |          |      |   | Y=- |     |                 |
|          |      |   |          | XY = |   | 3.5 |     |                 |
|          |      |   |          | 14.3 |   |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| Scin     |      |   | CFRP     | X =  |   | X=1 | 0   | Page 77, Note 6 |
| tillator |      |   | T300     | 1    |   | 7.4 | .12 | Margin of       |
| supports |      |   | Fabric   | 15.9 |   | Y=3 |     | safety          |
|          |      |   |          |      |   | 0.5 |     |                 |
|          |      |   |          | Y =  |   | XY= |     | Note 7          |
|          |      |   |          | 1    |   | 5.9 |     |                 |
|          |      |   |          | 15.9 |   |     |     |                 |
|          |      |   |          |      |   |     |     |                 |
|          |      |   |          | XY = |   |     |     |                 |
|          |      |   |          | 14.3 |   |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| **Margin |      |   |          |      |   |     |     |                 |
| of       |      |   |          |      |   |     |     |                 |
| Safety   |      |   |          |      |   |     |     |                 |
| Summary  |      |   |          |      |   |     |     |                 |
| of       |      |   |          |      |   |     |     |                 |
| AMS-02   |      |   |          |      |   |     |     |                 |
| Ring     |      |   |          |      |   |     |     |                 |
| Imaging  |      |   |          |      |   |     |     |                 |
| Chernkov |      |   |          |      |   |     |     |                 |
| Counter  |      |   |          |      |   |     |     |                 |
| (RICH)** |      |   |          |      |   |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| Item     | Dra  |   | Material | Mate |   | M   | Mar | Comments        |
|          | wing |   | and      | rial |   | ax. | gin |                 |
|          | nu   |   | temper   | a    |   | a   | of  |                 |
|          | mber |   |          | llow |   | ppl | Saf |                 |
|          |      |   |          | able |   | ied | ety |                 |
|          |      |   |          | st   |   | t   | (u  |                 |
|          |      |   |          | ress |   | ens | lt) |                 |
|          |      |   |          | (    |   | ile | FS= |                 |
|          |      |   |          | ksi) |   | str | 2.0 |                 |
|          |      |   |          |      |   | ess |     |                 |
|          |      |   |          |      |   | (k  |     |                 |
|          |      |   |          |      |   | si) |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| External |      |   |          |      |   |     |     |                 |
| S        |      |   |          |      |   |     |     |                 |
| tructure |      |   |          |      |   |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| Primary  |      |   | 70       | 64   |   | 1   | 1   | Page 47, Note 8 |
| beam     |      |   | 75-T7351 |      |   | 2.7 | .51 |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| S        |      |   | 70       | 64   |   | 1   | 1   | Page 47, Note 8 |
| econdary |      |   | 75-T7351 |      |   | 4.2 | .26 |                 |
| Internal |      |   |          |      |   |     |     |                 |
| beam     |      |   |          |      |   |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| Internal |      |   |          |      |   |     |     |                 |
| S        |      |   |          |      |   |     |     |                 |
| tructure |      |   |          |      |   |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| St       | 12   |   | 70       | 64   |   | 9.0 | \>  | Page 47, Note 8 |
| ructural | -RIC |   | 75-T7351 |      |   |     | 2.0 |                 |
| members  | SYS- |   |          |      |   |     |     |                 |
|          | 10   |   |          |      |   |     |     |                 |
|          | -001 |   |          |      |   |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| St       | 12   |   | 6061-T6  | 39.5 |   | 1   | 0   | Page 47, Note 8 |
| ructural | -RIC |   |          |      |   | 3.3 | .48 |                 |
| members  | SYS- |   |          |      |   |     |     |                 |
|          | 20   |   |          |      |   |     |     |                 |
|          | -002 |   |          |      |   |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| R        | 12   |   | 70       | 64   |   | 8   | \>  | Page 47, Note 8 |
| eflector | -RIC |   | 75-T7351 |      |   | .20 | 2.0 |                 |
| Support  | SYS- |   |          |      |   |     |     |                 |
|          | 40   |   |          |      |   |     |     |                 |
|          | -001 |   |          |      |   |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| R        | 13   |   | CFRP     | 6    |   | X=  | \>  | Page 48, Note   |
| eflector | -RIC |   | BRYTE    | 8.6, |   | 2.1 | 2.0 | 8, Margin of    |
|          | SYS- |   | EX-1515  | 6    |   | Y=  |     | safety          |
|          | 00   |   |          | 8.6, |   | 1.9 |     |                 |
|          | -008 |   |          | 27.2 |   | XY= |     | Note 9          |
|          |      |   |          |      |   | 1.1 |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| **Margin |      |   |          |      |   |     |     |                 |
| of       |      |   |          |      |   |     |     |                 |
| Safety   |      |   |          |      |   |     |     |                 |
| summary  |      |   |          |      |   |     |     |                 |
| of       |      |   |          |      |   |     |     |                 |
| AMS-02   |      |   |          |      |   |     |     |                 |
| Electro  |      |   |          |      |   |     |     |                 |
| Magnetic |      |   |          |      |   |     |     |                 |
| Cal      |      |   |          |      |   |     |     |                 |
| orimeter |      |   |          |      |   |     |     |                 |
| (ECAL)** |      |   |          |      |   |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| Item     | Dra  |   | Material | Mate |   | M   | Mar | Comments        |
|          | wing |   | and      | rial |   | ax. | gin |                 |
|          | nu   |   | temper   | a    |   | a   | of  |                 |
|          | mber |   |          | llow |   | ppl | Saf |                 |
|          |      |   |          | able |   | ied | ety |                 |
|          |      |   |          | st   |   | str | (u  |                 |
|          |      |   |          | ress |   | ess | lt) |                 |
|          |      |   |          | (    |   | (k  | FS= |                 |
|          |      |   |          | ksi) |   | si) | 1.4 |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| H        | ECA  |   | 2024-T4  | 61   |   | 16  | 1   | Page 27, Note   |
| oneycomb | L0-1 |   | (        |      |   | .0  | .73 | 10              |
| Face     | 0-Je |   | 2A12-T4) |      |   |     |     |                 |
| plate    |      |   |          |      |   |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| H        | ECA  |   | 2014-T6  | 6    |   | 2   | 1   | Page 27, Note   |
| oneycomb | L0-1 |   | (        | 5.3  |   | 1.3 | .19 | 10              |
| I frame  | 1-Je |   | 2A14-T6) |      |   |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| Side     | ECA  |   | 2014-T6  | 6    |   | 2   | 1   | Page 27, Note   |
| panels   | L0-2 |   | (        | 5.3  |   | 1.9 | .13 | 10              |
|          | 0-Je |   | 2A14-T6) |      |   |     |     |                 |
|          | ECA  |   |          |      |   |     |     |                 |
|          | L0-3 |   |          |      |   |     |     |                 |
|          | 0-Je |   |          |      |   |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| Bracket  | ECAL |   | 70       | 6    |   | 2   | 1   | Page 27, Note   |
|          | 0-41 |   | 50-T7451 | 9.9  |   | 1.0 | .37 | 10              |
|          | -Je  |   |          |      |   |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| Support  | ECAL |   | 70       | 6    |   | 4   | 0   | Page 27, Note   |
| beam     | 0-42 |   | 50-T7451 | 9.9  |   | 1.2 | .21 | 10              |
|          | -Je  |   |          |      |   |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| **Margin |      |   |          |      |   |     |     |                 |
| of       |      |   |          |      |   |     |     |                 |
| Safety   |      |   |          |      |   |     |     |                 |
| Summary  |      |   |          |      |   |     |     |                 |
| of       |      |   |          |      |   |     |     |                 |
| AMS-02   |      |   |          |      |   |     |     |                 |
| Star     |      |   |          |      |   |     |     |                 |
| T        |      |   |          |      |   |     |     |                 |
| racker** |      |   |          |      |   |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| Item     | Dra  |   | M        | Mate |   | M   | M   | Comments        |
|          | wing |   | aterials | rial |   | ax. | .S. |                 |
|          | nu   |   | and      | a    |   | li  | (u  |                 |
|          | mber |   | temper   | llow |   | mit | lt) |                 |
|          |      |   |          | able |   | str | FS= |                 |
|          |      |   |          | st   |   | ess | 2.0 |                 |
|          |      |   |          | ress |   | (K  |     |                 |
|          |      |   |          | (    |   | si) |     |                 |
|          |      |   |          | ksi) |   |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| Upper    |      |   | CFRP     | 154  |   | 43  | 0   | Page 13, Note   |
| bracket  |      |   | M55J     |      |   |     | .41 | 11, M.S. Note   |
|          |      |   | A        |      |   |     |     | 11a             |
|          |      |   | CGLTM110 |      |   |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| Lower    |      |   | CFRP     | 154  |   | 3   | 0   | Page 13, Note   |
| bracket  |      |   | M55J     |      |   | 1.6 | .11 | 11, M.S,. Note  |
|          |      |   | A        |      |   |     |     | 11a             |
|          |      |   | CGLTM110 |      |   |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| Baffle   |      |   | 70       | 59   |   | 2   | 0   | Page 11, Note   |
| to M     |      |   | 75-T7351 |      |   | 9.2 | .01 | 12              |
| s        |      |   |          |      |   |     |     |                 |
| tructure |      |   |          |      |   |     |     |                 |
| bracket  |      |   |          |      |   |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| **Margin |      |   |          |      |   |     |     |                 |
| of       |      |   |          |      |   |     |     |                 |
| Safety   |      |   |          |      |   |     |     |                 |
| Summary  |      |   |          |      |   |     |     |                 |
| of       |      |   |          |      |   |     |     |                 |
| AMS-02   |      |   |          |      |   |     |     |                 |
| Silicon  |      |   |          |      |   |     |     |                 |
| Tracker  |      |   |          |      |   |     |     |                 |
| Str      |      |   |          |      |   |     |     |                 |
| ucture** |      |   |          |      |   |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| Item     | Dra  |   | Material | Mate |   | M   | Mar | Comments        |
|          | wing |   | and      | rial |   | ax. | gin |                 |
|          | nu   |   | temper   | a    |   | a   | of  |                 |
|          | mber |   |          | llow |   | ppl | Saf |                 |
|          |      |   |          | able |   | ied | ety |                 |
|          |      |   |          | st   |   | t   | (u  |                 |
|          |      |   |          | ress |   | ens | lt) |                 |
|          |      |   |          | (    |   | ile | FS= |                 |
|          |      |   |          | ksi) |   | str | 2.0 |                 |
|          |      |   |          |      |   | ess |     |                 |
|          |      |   |          |      |   | (k  |     |                 |
|          |      |   |          |      |   | si) |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| Tracker  |      |   |          |      |   |     |     |                 |
| Outer    |      |   |          |      |   |     |     |                 |
| Planes   |      |   |          |      |   |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| Sandwich | AMS  |   | Carbon   | 50.7 |   | fx  | \>  | Page 22 Note 13 |
| facing   | II   |   | fiber    |      |   | =0. | 2.0 |                 |
|          | 154  |   | M60 J    |      |   | 536 |     |                 |
|          | A0   |   | Cyanate  |      |   | fy  |     |                 |
|          | AMS  |   | Ester    |      |   | =0. |     |                 |
|          | II   |   |          |      |   | 826 |     |                 |
|          | 155  |   |          |      |   | fxy |     |                 |
|          | A0   |   |          |      |   | =0. |     |                 |
|          |      |   |          |      |   | 276 |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| Sandwich | AMS  |   | Hexcel   | 0.11 |   | 0.  | 16  | Page 22 Note 13 |
| core     | II   |   | H        |      |   | 004 |     |                 |
|          | 154  |   | oneycomb |      |   |     |     |                 |
|          | A0   |   | 3/16 in. |      |   |     |     |                 |
|          | AMS  |   | Al. 5056 |      |   |     |     |                 |
|          | II   |   |          |      |   |     |     |                 |
|          | 155  |   |          |      |   |     |     |                 |
|          | A0   |   |          |      |   |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| Tracker  |      |   |          |      |   |     |     |                 |
| Inner    |      |   |          |      |   |     |     |                 |
| Planes   |      |   |          |      |   |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| Sandwich |      |   | Hexcel   | 0    |   | 0.  | 0   | Page 27 Note 13 |
| core     |      |   | H        | .025 |   | 011 | .12 |                 |
|          |      |   | oneycomb |      |   |     |     |                 |
|          |      |   | 3/8 in   |      |   |     |     |                 |
|          |      |   | Al. 5056 |      |   |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| Sandwich |      |   | Carbon   | 72.5 |   | f   | 4.8 | Page 27 Note 13 |
| facing   |      |   | fiber    |      |   | x=4 |     |                 |
|          |      |   | M60 J    |      |   | .06 |     |                 |
|          |      |   | Cyanate  |      |   | f   |     |                 |
|          |      |   | Ester    |      |   | y=3 |     |                 |
|          |      |   |          |      |   | .33 |     |                 |
|          |      |   |          |      |   | fx  |     |                 |
|          |      |   |          |      |   | y=1 |     |                 |
|          |      |   |          |      |   | .65 |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| Insert   |      |   | Hexcel   | 0.11 |   | 0.  | 1   | Page 27 Note 13 |
| ring     |      |   | H        |      |   | 024 | .26 |                 |
| core     |      |   | oneycomb |      |   |     |     |                 |
|          |      |   | 3/16 in. |      |   |     |     |                 |
|          |      |   | Al. 5056 |      |   |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| Tracker  |      |   | T        | 130  |   | 5   | 0   | Page 5, Note 14 |
| feet     |      |   | i-6Al-4V |      |   | 6.4 | .14 |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| **Margin |      |   |          |      |   |     |     |                 |
| of       |      |   |          |      |   |     |     |                 |
| Safety   |      |   |          |      |   |     |     |                 |
| Summary  |      |   |          |      |   |     |     |                 |
| of       |      |   |          |      |   |     |     |                 |
| AMS-02   |      |   |          |      |   |     |     |                 |
| Cryo     |      |   |          |      |   |     |     |                 |
| magnet** |      |   |          |      |   |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| Item     | Dra  |   | Material | Mate |   | M   | Mar | Comments        |
|          | wing |   | and      | rial |   | ax. | gin |                 |
|          | Nu   |   | temper   | a    |   | a   | of  |                 |
|          | mber |   |          | llow |   | ppl | Saf |                 |
|          |      |   |          | able |   | ied | ety |                 |
|          |      |   |          | st   |   | t   | (u  |                 |
|          |      |   |          | ress |   | ens | lt) |                 |
|          |      |   |          | (    |   | ile | FS  |                 |
|          |      |   |          | ksi) |   | str | =1  |                 |
|          |      |   |          |      |   | ess | .50 |                 |
|          |      |   |          |      |   | (k  |     |                 |
|          |      |   |          |      |   | si) |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| Race     | SCD  |   | 6061-T6  | 53.7 |   | 2   | 0   | Page 7,         |
| track    | 0825 |   | (10 in)  |      |   | 9.4 | .22 | sect.1.1.1 Note |
| End      |      |   | 1.8 K    |      |   |     |     | 15              |
| frame    |      |   |          |      |   |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| Dipole   | SCD  |   | 6061-T6  | 53.7 |   | 2   | 0   | Page 8,         |
| Island   | 0810 |   | (10 in)  |      |   | 9.0 | .23 | sect.1.1.2 c    |
|          |      |   | 1.8 K    |      |   |     |     | Note 15         |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| Race     | SCD  |   | 6061-T6  | 53.7 |   | 1   | 0   | Page 8,         |
| track    | 0841 |   | (10 in)  |      |   | 9.6 | .83 | sect.1.1.2 b    |
| coils    |      |   | 1.8 K    |      |   |     |     | Note 15         |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| Race     | S    |   | 2        | 60.9 |   | 2   | 0   | Page 13, sect   |
| track    | CD08 |   | 219-T851 |      |   | 7.6 | .47 | 1.1.5 a, max.   |
| edge     | 51-4 |   | (300 K)  |      |   |     |     | tens stress     |
| plate    |      |   |          |      |   |     |     | preload warm,   |
| outer    |      |   |          |      |   |     |     | Note 15         |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| Race     | S    |   | 6061-T6  | 36.9 |   | 2   | 0   | Page 13, sect   |
| track    | CD08 |   | (10 in)  |      |   | 1.6 | .14 | 1.1.5 b, max.   |
| edge     | 51-3 |   | (300K)   |      |   |     |     | tens stress     |
| plate    |      |   |          |      |   |     |     | preload warm,   |
| curved   |      |   |          |      |   |     |     | Note 15         |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| Dipole   | SC   |   | 6061-T6  | 36.9 |   | 2   | 0   | Page 14, sect   |
| edge     | D081 |   | (10 in)  |      |   | 2.5 | .10 | 1.1.5 c, max.   |
| Plate    | 2-01 |   | (300K)   |      |   |     |     | tens            |
|          |      |   |          |      |   |     |     |                 |
|          |      |   |          |      |   |     |     | stress preload  |
|          |      |   |          |      |   |     |     | warm, Note 15   |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| Helium   | SC   |   | 316 Hi   | 2    |   | 14  | 0   | Page 48, sect   |
| vessel   | D088 |   | proof    | 32.1 |   | 3.6 | .08 | 4.1.d inertia   |
| Fx       | 9-02 |   | s        |      |   |     |     | loads,          |
| support  |      |   | tainless |      |   |     |     |                 |
| pin      |      |   | steel    |      |   |     |     | Note 15         |
|          |      |   | (4K)     |      |   |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| Helium   | SC   |   | 316 Hi   | 31.9 |   | 2   | 0   | Page 49, sect   |
| vessel   | D091 |   | proof    |      |   | 0.5 | .42 | 4.2.A inertia   |
| Fy       | 0-01 |   | s        |      |   |     | yi  | loads,          |
| support  |      |   | tainless |      |   |     | eld |                 |
| pin      |      |   | steel    |      |   |     |     | Note 15         |
|          |      |   | (4K)     |      |   |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| Helium   | SC   |   | 316 Hi   | 2    |   | 13  | 0   | Page 54, sect   |
| vessel   | D089 |   | proof    | 32.1 |   | 0.7 | .18 | 4.4.C inertia   |
| Fz       | 8-01 |   | s        |      |   |     |     | loads,          |
| support  |      |   | tainless |      |   |     |     |                 |
| pin      |      |   | steel    |      |   |     |     | Note 15         |
|          |      |   | (4K)     |      |   |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| **Margin |      |   |          |      |   |     |     |                 |
| of       |      |   |          |      |   |     |     |                 |
| Safety   |      |   |          |      |   |     |     |                 |
| Summary  |      |   |          |      |   |     |     |                 |
| of       |      |   |          |      |   |     |     |                 |
| AMS-02   |      |   |          |      |   |     |     |                 |
| Helium   |      |   |          |      |   |     |     |                 |
| Tank**   |      |   |          |      |   |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| Item     | Dra  |   | Material | Mate |   | M   | Mar | Comments        |
|          | wing |   | and      | rial |   | ax. | gin |                 |
|          | nu   |   | temper   | a    |   | a   | of  |                 |
|          | mber |   |          | llow |   | ppl | Saf |                 |
|          |      |   |          | able |   | ied | ety |                 |
|          |      |   |          | y    |   | yi  | (u  |                 |
|          |      |   |          | ield |   | eld | lt) |                 |
|          |      |   |          | st   |   | str | FS= |                 |
|          |      |   |          | ress |   | ess | 2.0 |                 |
|          |      |   |          | (    |   | (k  |     |                 |
|          |      |   |          | ksi) |   | si) |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| Central  | SCD  |   | 5        | 2    |   | 21  | 0.0 | Page 3-7, Note  |
| Ring     | 090  |   | 083-H111 | 6.49 |   | .19 | 003 | 16 (bearing     |
|          | 5-01 |   | forging  |      |   |     |     | yield)          |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| Thru     | SCD  |   | 5        | 3    |   | 27  | 0   | Page 3-12, Note |
| tube     | 090  |   | 083-H321 | 5.67 |   | .24 | .05 | 16 (yield)      |
|          | 2-01 |   | cold     |      |   |     |     |                 |
|          |      |   | worked   |      |   |     |     |                 |
|          | SCD  |   | forging  |      |   |     |     |                 |
|          | 090  |   |          |      |   |     |     |                 |
|          | 3-01 |   |          |      |   |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| Outer    | SCD  |   | 5        | 2    |   | 5   | 2   | Page3-19, Note  |
| ring     | 090  |   | 083-H321 | 2.09 |   | .16 | .42 | 16 (yield )     |
| weld     | 5-02 |   |          |      |   |     |     |                 |
|          | ,-03 |   |          |      |   |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| Inner    | SCD  |   | 5        | 2    |   | 2   | 0   | Page 3-16, Note |
| ring     | 090  |   | 083-H321 | 3.46 |   | 0.3 | .69 | 16 (yield)      |
| weld     | 5-04 |   |          |      |   |     |     |                 |
|          | ,-05 |   |          |      |   |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| Central  | SCD  |   | 5        | 2    |   | 16  | 0   | Page3-35, Note  |
| plate    | 090  |   | 083-H321 | 5.20 |   | .71 | .21 | 16 (yield)      |
| weld     | 5-01 |   |          |      |   |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| Central  | SCD  |   | 5        | 2    |   | 1   | 0   | Page 3-7, Note  |
| Ring     | 090  |   | 083-H111 | 5.20 |   | 6.0 | .26 | 16 (yield)      |
| weld     | 5-01 |   | forging  |      |   |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| **Margin |      |   |          |      |   |     |     |                 |
| of       |      |   |          |      |   |     |     |                 |
| Safety   |      |   |          |      |   |     |     |                 |
| of       |      |   |          |      |   |     |     |                 |
| AMS-02   |      |   |          |      |   |     |     |                 |
| Cr       |      |   |          |      |   |     |     |                 |
| yomagnet |      |   |          |      |   |     |     |                 |
| Su       |      |   |          |      |   |     |     |                 |
| spension |      |   |          |      |   |     |     |                 |
| Straps** |      |   |          |      |   |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| Item     | Dra  |   | Material | Mate |   | M   | Mar | Comments        |
|          | wing |   | and      | rial |   | ax. | gin |                 |
|          | Nu   |   | temper   | a    |   | a   | of  |                 |
|          | mber |   |          | llow |   | ppl | Saf |                 |
|          |      |   |          | able |   | ied | ety |                 |
|          |      |   |          | st   |   | t   | (u  |                 |
|          |      |   |          | ress |   | ens | lt) |                 |
|          |      |   |          | (    |   | ile | FS  |                 |
|          |      |   |          | ksi) |   | str | =1  |                 |
|          |      |   |          |      |   | ess | .40 |                 |
|          |      |   |          |      |   | (k  |     |                 |
|          |      |   |          |      |   | si) |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| Race     | SCD  |   | 6061-T6  | 2    |   | 6   | 0.  | Page 7, Note 17 |
| track    | 0825 |   | (10 in)  | 0087 |   | 503 | 109 |                 |
| end      |      |   |          | lbs  |   | lbs |     |                 |
| frame    |      |   |          | (ax  |   | (   |     |                 |
| clevis   |      |   |          | ial) |   | axi |     |                 |
| C1       |      |   |          |      |   | al) |     |                 |
| W1clevis |      |   |          | 1    |   |     |     |                 |
|          |      |   |          | 3986 |   | 6   |     |                 |
|          |      |   |          | lbs  |   | 995 |     |                 |
|          |      |   |          |      |   | lbs |     |                 |
|          |      |   |          | (tra |   |     |     |                 |
|          |      |   |          | nsve |   | (tr |     |                 |
|          |      |   |          | rse) |   | ans |     |                 |
|          |      |   |          |      |   | ver |     |                 |
|          |      |   |          |      |   | se) |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| Race     | SCD  |   | 316L     | 12   |   | 85  | 0.  | Page 13, Note   |
| track    | 067  |   | Hi-Proof | 7.64 |   | .77 | 063 | 17              |
| end      | 8-02 |   | s        |      |   |     |     |                 |
| frame    |      |   | tainless |      |   |     |     |                 |
| clevis   |      |   | steel    |      |   |     |     |                 |
| pin C1W1 |      |   |          |      |   |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| Carbon   | SCD  |   | Carbon   | 27   |   | 117 | 0   | Page 6, Note    |
| Band     | 067  |   | Fiber    | 5.58 |   | .77 | .67 | 18,             |
|          | 8-03 |   | epoxy    |      |   |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| FGR Band | SCD  |   | FGR3     | 26   |   | 59  | 2   | Page 7,Note 18  |
|          | 067  |   | epoxy    | 1.07 |   | .32 | .14 |                 |
|          | 8-12 |   |          |      |   |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| Glass    | SCD  |   | S2 glass | 21   |   | 61  | 1   | Page 7,Note 18  |
| Band     | 067  |   | epoxy    | 7.56 |   | .28 | .54 |                 |
|          | 8-11 |   |          |      |   |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| Glass    | SCD  |   | S2 glass | 21   |   | 98  | 0   | Page 7,Note 18  |
| Bod      | 067  |   | epoxy    | 7.56 |   | .38 | .58 |                 |
|          | 8-18 |   |          |      |   |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| **Margin |      |   |          |      |   |     |     |                 |
| of       |      |   |          |      |   |     |     |                 |
| Safety   |      |   |          |      |   |     |     |                 |
| of       |      |   |          |      |   |     |     |                 |
| AMS-02   |      |   |          |      |   |     |     |                 |
| Anti     |      |   |          |      |   |     |     |                 |
| Coi      |      |   |          |      |   |     |     |                 |
| ncidence |      |   |          |      |   |     |     |                 |
| Counter  |      |   |          |      |   |     |     |                 |
| (ACC)**  |      |   |          |      |   |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| Item     | Dra  |   | Material | Mate | M |     | Mar | Comments        |
|          | wing |   | and      | rial | a |     | gin |                 |
|          | Nu   |   | temper   | a    | x |     | of  |                 |
|          | mber |   |          | llow | . |     | Saf |                 |
|          |      |   |          | able | a |     | ety |                 |
|          |      |   |          | st   | p |     | (u  |                 |
|          |      |   |          | ress | p |     | lt) |                 |
|          |      |   |          | (    | l |     | FS  |                 |
|          |      |   |          | ksi) | i |     | =   |                 |
|          |      |   |          |      | e |     | 2.0 |                 |
|          |      |   |          |      | d |     |     |                 |
|          |      |   |          |      | s |     |     |                 |
|          |      |   |          |      | t |     |     |                 |
|          |      |   |          |      | r |     |     |                 |
|          |      |   |          |      | e |     |     |                 |
|          |      |   |          |      | s |     |     |                 |
|          |      |   |          |      | s |     |     |                 |
|          |      |   |          |      | ( |     |     |                 |
|          |      |   |          |      | k |     |     |                 |
|          |      |   |          |      | s |     |     |                 |
|          |      |   |          |      | i |     |     |                 |
|          |      |   |          |      | ) |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| ACC      | a    |   | 70       | 56   | 2 |     | 0   | Page 13, Note   |
| Clamps   | ms-0 |   | 75-T7351 |      | 5 |     | .09 | 19              |
|          | 2-03 |   |          |      | . |     |     |                 |
|          | 1024 |   |          |      | 8 |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| ACC      | am   |   | CFRP     | 211  | 0 |     | \>  |                 |
| cylinder | s-02 |   | Tenax J  |      | . |     | 2.0 |                 |
|          | 1626 |   | UMS2526  |      | 0 |     |     |                 |
|          |      |   |          |      | 7 |     |     |                 |
|          |      |   |          |      | 4 |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| ACC      | am   |   | Bicron   | 4.5  | 0 |     | \>  |                 |
| panels   | s-02 |   | BC 414   |      | . |     | 2.0 |                 |
|          | 1    |   | P        |      | 2 |     |     |                 |
|          | 771c |   | olyvinyl |      | 2 |     |     |                 |
|          |      |   | Toluene  |      |   |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| C        | 1    |   | 70       | 68   | 2 |     | 0   | Page 17, Note   |
| onnector | 812/ |   | 75-T7351 |      | 2 |     | .54 | 31              |
| support  | 60\_ |   |          |      |   |     |     |                 |
|          | 0    |   |          |      |   |     |     |                 |
|          | 004_ |   |          |      |   |     |     |                 |
|          | I_VI |   |          |      |   |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| ACC PMT  | 1    |   | 70       | 67   | 0 |     | \>  | Note 19         |
| support  | 812/ |   | 75-T7351 |      | . |     | 2.0 |                 |
|          | 60\_ |   |          |      | 1 |     |     |                 |
|          | 0    |   |          |      | 3 |     |     |                 |
|          | 010_ |   |          |      |   |     |     |                 |
|          | I_VI |   |          |      |   |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| **Margin |      |   |          |      |   |     |     |                 |
| of       |      |   |          |      |   |     |     |                 |
| Safety   |      |   |          |      |   |     |     |                 |
| Summary  |      |   |          |      |   |     |     |                 |
| of       |      |   |          |      |   |     |     |                 |
| Zenith   |      |   |          |      |   |     |     |                 |
| Ra       |      |   |          |      |   |     |     |                 |
| diator** |      |   |          |      |   |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| Item     | Dra  |   | Material | Mate | M |     | Mar | Comments        |
|          | wing |   | and      | rial | a |     | gin |                 |
|          | Nu   |   | temper   | a    | x |     | of  |                 |
|          | mber |   |          | llow | . |     | Saf |                 |
|          |      |   |          | able | a |     | ety |                 |
|          |      |   |          | st   | p |     | (u  |                 |
|          |      |   |          | ress | p |     | lt) |                 |
|          |      |   |          | (    | l |     | FS  |                 |
|          |      |   |          | ksi) | i |     | =   |                 |
|          |      |   |          |      | e |     | 2.0 |                 |
|          |      |   |          |      | d |     |     |                 |
|          |      |   |          |      | t |     |     |                 |
|          |      |   |          |      | e |     |     |                 |
|          |      |   |          |      | n |     |     |                 |
|          |      |   |          |      | s |     |     |                 |
|          |      |   |          |      | i |     |     |                 |
|          |      |   |          |      | l |     |     |                 |
|          |      |   |          |      | e |     |     |                 |
|          |      |   |          |      | s |     |     |                 |
|          |      |   |          |      | t |     |     |                 |
|          |      |   |          |      | r |     |     |                 |
|          |      |   |          |      | e |     |     |                 |
|          |      |   |          |      | s |     |     |                 |
|          |      |   |          |      | s |     |     |                 |
|          |      |   |          |      | ( |     |     |                 |
|          |      |   |          |      | k |     |     |                 |
|          |      |   |          |      | s |     |     |                 |
|          |      |   |          |      | i |     |     |                 |
|          |      |   |          |      | ) |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| Radiator | AM   |   | Rohacell | 0    | 0 |     | 0   | Page 52, Note   |
| panels   | S-01 |   | core     | .100 | . |     | .01 | 20, EVA load    |
|          | .10. |   | 2024-T81 |      | 0 |     |     | case            |
|          | 10   |   | face     |      | 4 |     |     |                 |
|          | .000 |   | sheets   |      | 9 |     |     |                 |
|          |      |   |          |      | 7 |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| 3W       | AM   |   | 70       | 59.9 | 2 |     | 0   | Page 43, Note   |
| i        | S-01 |   | 75-T7351 |      | 6 |     | .12 | 20 ,            |
| nterface | .00. |   |          |      | . |     |     | Liftoff/landing |
| bracket  | 00   |   |          |      | 7 |     |     | cases           |
|          | .002 |   |          |      |   |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| I        | AM   |   | Carbon   | 87   | 3 |     | 0   | Page 63, Note   |
| nterface | S-01 |   | fiber    |      | 5 |     | .23 | 20 , Thermal    |
| Spokes   | .30. |   |          |      | . |     |     | induced         |
|          | 00   |   |          |      | 4 |     |     |                 |
|          | .003 |   |          |      |   |     |     | Load cases      |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| **Margin |      |   |          |      |   |     |     |                 |
| of       |      |   |          |      |   |     |     |                 |
| Safety   |      |   |          |      |   |     |     |                 |
| Summary  |      |   |          |      |   |     |     |                 |
| of Main  |      |   |          |      |   |     |     |                 |
| and      |      |   |          |      |   |     |     |                 |
| Tracker  |      |   |          |      |   |     |     |                 |
| Ra       |      |   |          |      |   |     |     |                 |
| diator** |      |   |          |      |   |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| Item     | Dra  |   | Material | Mate | M |     | Mar | Comments        |
|          | wing |   | and      | rial | a |     | gin |                 |
|          | Nu   |   | temper   | a    | x |     | of  |                 |
|          | mber |   |          | llow | . |     | Saf |                 |
|          |      |   |          | able | a |     | ety |                 |
|          |      |   |          | st   | p |     | (u  |                 |
|          |      |   |          | ress | p |     | lt) |                 |
|          |      |   |          | (    | l |     | FS  |                 |
|          |      |   |          | ksi) | i |     | =   |                 |
|          |      |   |          |      | e |     | 2.0 |                 |
|          |      |   |          |      | d |     |     |                 |
|          |      |   |          |      | t |     |     |                 |
|          |      |   |          |      | e |     |     |                 |
|          |      |   |          |      | n |     |     |                 |
|          |      |   |          |      | s |     |     |                 |
|          |      |   |          |      | i |     |     |                 |
|          |      |   |          |      | l |     |     |                 |
|          |      |   |          |      | e |     |     |                 |
|          |      |   |          |      | s |     |     |                 |
|          |      |   |          |      | t |     |     |                 |
|          |      |   |          |      | r |     |     |                 |
|          |      |   |          |      | e |     |     |                 |
|          |      |   |          |      | s |     |     |                 |
|          |      |   |          |      | s |     |     |                 |
|          |      |   |          |      | ( |     |     |                 |
|          |      |   |          |      | k |     |     |                 |
|          |      |   |          |      | s |     |     |                 |
|          |      |   |          |      | i |     |     |                 |
|          |      |   |          |      | ) |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| Main     | 21-A |   | 6063-T5  | 2    | 7 |     | 0   | Pages189 --     |
| radiator | MS-0 |   |          | 5.35 | . |     | .54 | 191,Note 22.    |
| panel    | 00.0 |   |          |      | 7 |     |     |                 |
| heat     | 0.XY |   |          |      |   |     |     |                 |
| pipes    | &    |   |          |      |   |     |     |                 |
|          | 22-A |   |          |      |   |     |     |                 |
|          | MS-0 |   |          |      |   |     |     |                 |
|          | 00.0 |   |          |      |   |     |     |                 |
|          | 0.XY |   |          |      |   |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| Tracker  | 25-A |   | 6063-T5  | 2    | 1 |     | 0   | Pages 192-195,  |
| radiator | MS-0 |   |          | 5.35 | 2 |     | .39 | Note 22         |
| panel    | 00.0 |   |          |      | . |     |     |                 |
| heat     | 0.XY |   |          |      | 8 |     |     |                 |
| pipes    |      |   |          |      | 2 |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| Main /   | 2    |   | 7075-T73 | 6    | 2 |     | 0   | Page 198, Note  |
| Tracker  | 4-AM |   |          | 2.97 | 7 |     | .15 | 22              |
| radiator | S-33 |   |          |      | . |     |     |                 |
| bracket  | 0.08 |   |          |      | 4 |     |     |                 |
|          | .XY  |   |          |      | 6 |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| Tracker  |      |   | Carbon   | 1022 | 2 |     | 0   | Page 188 &197,  |
| radiator |      |   | fiber    | lbf  | 6 |     | .92 | Note 22         |
| rod 4    |      |   |          |      | 6 |     |     |                 |
|          |      |   |          |      | l |     |     |                 |
|          |      |   |          |      | b |     |     |                 |
|          |      |   |          |      | f |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| Main     | 2    |   | 2024-T81 | 6    | 1 |     | 0   | Page 196, Note  |
| Radiator | 1_AM |   |          | 2.97 | 7 |     | .78 | 22              |
| Skin     | S-00 |   |          |      | . |     |     |                 |
|          | 0.00 |   |          |      | 6 |     |     |                 |
|          | .XY, |   |          |      | 8 |     |     |                 |
|          | 22-A |   |          |      |   |     |     |                 |
|          | MS-0 |   |          |      |   |     |     |                 |
|          | 00.0 |   |          |      |   |     |     |                 |
|          | 0.XY |   |          |      |   |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| Tracker  | 2    |   | 2024-T81 | 6    | 2 |     | 0   | Page 197, Note  |
| radiator | 5-AM |   |          | 2.97 | 7 |     | .14 | 22              |
| skin     | S-00 |   |          |      | . |     |     |                 |
|          | 0.00 |   |          |      | 6 |     |     |                 |
|          | .01, |   |          |      | 3 |     |     |                 |
|          |      |   |          |      |   |     |     |                 |
|          | 25-A |   |          |      |   |     |     |                 |
|          | MS-0 |   |          |      |   |     |     |                 |
|          | 00-0 |   |          |      |   |     |     |                 |
|          | 0.02 |   |          |      |   |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| **Margin |      |   |          |      |   |     |     |                 |
| of       |      |   |          |      |   |     |     |                 |
| Safety   |      |   |          |      |   |     |     |                 |
| of       |      |   |          |      |   |     |     |                 |
| AMS-02   |      |   |          |      |   |     |     |                 |
| El       |      |   |          |      |   |     |     |                 |
| ectronic |      |   |          |      |   |     |     |                 |
| Crates   |      |   |          |      |   |     |     |                 |
| and      |      |   |          |      |   |     |     |                 |
| Radiator |      |   |          |      |   |     |     |                 |
| Br       |      |   |          |      |   |     |     |                 |
| ackets** |      |   |          |      |   |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| Item     | Dra  |   | Material | Mate | M |     | Mar | Comments        |
|          | wing |   | and      | rial | a |     | gin |                 |
|          | Nu   |   | temper   | a    | x |     | of  |                 |
|          | mber |   |          | llow | . |     | Saf |                 |
|          |      |   |          | able | a |     | ety |                 |
|          |      |   |          | st   | p |     | (u  |                 |
|          |      |   |          | ress | p |     | lt) |                 |
|          |      |   |          | (    | l |     | FS  |                 |
|          |      |   |          | ksi) | i |     | =   |                 |
|          |      |   |          |      | e |     | 2.0 |                 |
|          |      |   |          |      | d |     |     |                 |
|          |      |   |          |      | t |     |     |                 |
|          |      |   |          |      | e |     |     |                 |
|          |      |   |          |      | n |     |     |                 |
|          |      |   |          |      | s |     |     |                 |
|          |      |   |          |      | i |     |     |                 |
|          |      |   |          |      | l |     |     |                 |
|          |      |   |          |      | e |     |     |                 |
|          |      |   |          |      | s |     |     |                 |
|          |      |   |          |      | t |     |     |                 |
|          |      |   |          |      | r |     |     |                 |
|          |      |   |          |      | e |     |     |                 |
|          |      |   |          |      | s |     |     |                 |
|          |      |   |          |      | s |     |     |                 |
|          |      |   |          |      | ( |     |     |                 |
|          |      |   |          |      | k |     |     |                 |
|          |      |   |          |      | s |     |     |                 |
|          |      |   |          |      | i |     |     |                 |
|          |      |   |          |      | ) |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| XPD      | 24-  |   | 70       | 5    | 2 |     | 0   | Page 198, Note  |
| s        | AMS- |   | 75-T7351 | 8.29 | 6 |     | .09 | 22              |
| tructure | 1    |   |          |      | . |     |     |                 |
|          | 20.A |   |          |      | 7 |     |     |                 |
|          | B.XY |   |          |      | 3 |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| Crate    | 24-  |   | 70       | 5    | 2 |     | 0   | Page 198, Note  |
| s        | AMS- |   | 75-T7351 | 8.29 | 8 |     | .03 | 22              |
| tructure | 1    |   |          |      | . |     |     |                 |
|          | 10.A |   |          |      | 2 |     |     |                 |
|          | B.XY |   |          |      | 2 |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| XPD      | 24-  |   | 6061-T6  | 3    | 2 |     | 0   | Page 173, Note  |
| board    | AMS- |   |          | 9.45 | 1 |     | .21 | 22              |
| st       | 1    |   |          |      | . |     |     |                 |
| iffeners | 21.0 |   |          |      | 7 |     |     |                 |
|          | 3.XY |   |          |      | 7 |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| Links    | 24-  |   | 70       | 5    | 2 |     | 0   | Page 198, Note  |
|          | AMS- |   | 75-T7351 | 3.58 | 0 |     | .33 | 22              |
|          | 1    |   |          |      | . |     |     |                 |
|          | 30.0 |   |          |      | 1 |     |     |                 |
|          | 1.XY |   |          |      | 6 |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| Top      | 24-  |   | 70       | 5    | 2 |     | 0   | Page 196, Note  |
| bracket  | AMS- |   | 75-T7351 | 3.58 | 4 |     | .09 | 22              |
|          | 3    |   |          |      | . |     |     |                 |
|          | 10.0 |   |          |      | 5 |     |     |                 |
|          | 2.XY |   |          |      | 5 |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| Mid      | 24-  |   | 70       | 5    | 2 |     | 0   | Page 196, Note  |
| bracket  | AMS- |   | 75-T7351 | 3.58 | 5 |     | .05 | 22              |
|          | 3    |   |          |      | . |     |     |                 |
|          | 20.0 |   |          |      | 4 |     |     |                 |
|          | 2.XY |   |          |      | 7 |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| Lower    | 24-  |   | 70       | 5    | 9 |     | \>  | Page 196, Note  |
| bracket  | AMS- |   | 75-T7351 | 6.41 | . |     | 2.0 | 22              |
|          | 3    |   |          |      | 1 |     |     |                 |
|          | 20.0 |   |          |      | 5 |     |     |                 |
|          | 2.XY |   |          |      |   |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| **Margin |      |   |          |      |   |     |     |                 |
| of       |      |   |          |      |   |     |     |                 |
| Safety   |      |   |          |      |   |     |     |                 |
| Summary  |      |   |          |      |   |     |     |                 |
| of High  |      |   |          |      |   |     |     |                 |
| Voltage  |      |   |          |      |   |     |     |                 |
| (HV)     |      |   |          |      |   |     |     |                 |
| Bricks** |      |   |          |      |   |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| Item     | Dra  |   | Material | Mate | M |     | Mar | Comments        |
|          | wing |   | and      | rial | a |     | gin |                 |
|          | Nu   |   | temper   | a    | x |     | of  |                 |
|          | mber |   |          | llow | . |     | Saf |                 |
|          |      |   |          | able | a |     | ety |                 |
|          |      |   |          | st   | p |     | (u  |                 |
|          |      |   |          | ress | p |     | lt) |                 |
|          |      |   |          | (    | l |     | FS  |                 |
|          |      |   |          | ksi) | i |     | =   |                 |
|          |      |   |          |      | e |     | 2.0 |                 |
|          |      |   |          |      | d |     |     |                 |
|          |      |   |          |      | t |     |     |                 |
|          |      |   |          |      | e |     |     |                 |
|          |      |   |          |      | n |     |     |                 |
|          |      |   |          |      | s |     |     |                 |
|          |      |   |          |      | i |     |     |                 |
|          |      |   |          |      | l |     |     |                 |
|          |      |   |          |      | e |     |     |                 |
|          |      |   |          |      | s |     |     |                 |
|          |      |   |          |      | t |     |     |                 |
|          |      |   |          |      | r |     |     |                 |
|          |      |   |          |      | e |     |     |                 |
|          |      |   |          |      | s |     |     |                 |
|          |      |   |          |      | s |     |     |                 |
|          |      |   |          |      | ( |     |     |                 |
|          |      |   |          |      | k |     |     |                 |
|          |      |   |          |      | s |     |     |                 |
|          |      |   |          |      | i |     |     |                 |
|          |      |   |          |      | ) |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| ECAL and |      |   |          |      |   |     |     |                 |
| RICH HV  |      |   |          |      |   |     |     |                 |
| Bricks   |      |   |          |      |   |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| Bracket  |      |   | 70       | 6    | 1 |     | 1   | Page 125, Note  |
|          |      |   | 75-T7351 | 3.8  | 4 |     | .17 | 23              |
|          |      |   |          |      | . |     |     |                 |
|          |      |   |          |      | 7 |     |     |                 |
|          |      |   |          |      |   |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| Frame    |      |   | 70       | 59.2 | 1 |     | 1.5 | Page 125, Note  |
|          |      |   | 75-T7351 |      | 1 |     |     | 23              |
|          |      |   |          |      | . |     |     |                 |
|          |      |   |          |      | 8 |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| Cover    |      |   | 6061-T62 | 39.5 | 6 |     | 1   | Page 125, Note  |
|          |      |   |          |      | . |     | .88 | 23              |
|          |      |   |          |      | 8 |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| Lateral  |      |   | 70       | 63.8 | 2 |     | 0   | Page 125, Note  |
| walls    |      |   | 75-T7351 |      | 3 |     | .34 | 23              |
|          |      |   |          |      | . |     |     |                 |
|          |      |   |          |      | 8 |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| TOF HV   |      |   |          |      |   |     |     |                 |
| bricks   |      |   |          |      |   |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| Frame    |      |   | 70       | 63.8 | 1 |     | 1   | Page 126, Note  |
|          |      |   | 75-T7351 |      | 1 |     | .75 | 23              |
|          |      |   |          |      | . |     |     |                 |
|          |      |   |          |      | 6 |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| Cover    |      |   | 6061-T62 | 39.5 | 1 |     | 0   | Page126, Note   |
|          |      |   |          |      | 4 |     | .41 | 23              |
|          |      |   |          |      | . |     |     |                 |
|          |      |   |          |      | 0 |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| Vertical |      |   | 70       | 63.8 | 1 |     | 1   | Page 126, Note  |
| Stand    |      |   | 75-T7351 |      | 1 |     | .68 | 23              |
| off      |      |   |          |      | . |     |     |                 |
|          |      |   |          |      | 9 |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| **Margin |      |   |          |      |   |     |     |                 |
| of       |      |   |          |      |   |     |     |                 |
| Safety   |      |   |          |      |   |     |     |                 |
| Summary  |      |   |          |      |   |     |     |                 |
| of       |      |   |          |      |   |     |     |                 |
| AMS-02   |      |   |          |      |   |     |     |                 |
| Vacuum   |      |   |          |      |   |     |     |                 |
| Case     |      |   |          |      |   |     |     |                 |
| Comp     |      |   |          |      |   |     |     |                 |
| onents** |      |   |          |      |   |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| Item     | Dra  |   | Material | Mate | M |     | Mar | Comments        |
|          | wing |   | and      | rial | a |     | gin |                 |
|          | nu   |   | temper   | a    | x |     | of  |                 |
|          | mber |   |          | llow | . |     | Saf |                 |
|          |      |   |          | able | a |     | ety |                 |
|          |      |   |          | st   | p |     | (u  |                 |
|          |      |   |          | ress | p |     | lt) |                 |
|          |      |   |          | (    | l |     | FS= |                 |
|          |      |   |          | ksi) | i |     | 1.4 |                 |
|          |      |   |          |      | e |     |     |                 |
|          |      |   |          |      | d |     |     |                 |
|          |      |   |          |      | s |     |     |                 |
|          |      |   |          |      | t |     |     |                 |
|          |      |   |          |      | r |     |     |                 |
|          |      |   |          |      | e |     |     |                 |
|          |      |   |          |      | s |     |     |                 |
|          |      |   |          |      | s |     |     |                 |
|          |      |   |          |      | ( |     |     |                 |
|          |      |   |          |      | k |     |     |                 |
|          |      |   |          |      | s |     |     |                 |
|          |      |   |          |      | i |     |     |                 |
|          |      |   |          |      | ) |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| Outer    | SDG  |   | 70       | 67   | 1 |     | 1   | Sect. 3.2.1-14, |
| Cylinder | 3913 |   | 50-T7452 |      | 8 |     | .32 | Note 26         |
|          | 5779 |   | Forging  |      | . |     |     |                 |
|          |      |   |          |      | 9 |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| Inner    | SDG  |   | 2        | 60   | 3 |     | 0   | Sect. 3.3.1-17, |
| Cylinder | 3913 |   | 219-T852 |      | 1 |     | .31 | Note 26         |
|          | 5782 |   | Forging  |      | . |     |     |                 |
|          |      |   |          |      | 4 |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| Inner    | SDG  |   | 2        | 32   | 1 |     | 0.  | Sect. 3.3.1-20, |
| cylinder | 3913 |   | 219-T852 |      | 9 |     | 116 | Note 26         |
| weld     | 5782 |   | Forging  |      | . |     |     |                 |
|          |      |   |          |      | 7 |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| Conical  | SDG  |   | 2219-T62 | 54   | 2 |     | 0   | Sect 3.1.1-14,  |
| flanges  | 3913 |   | Plate    |      | 8 |     | .30 | Note 26         |
|          | 5778 |   |          |      | . |     |     |                 |
|          |      |   |          |      | 7 |     | (0  |                 |
|          |      |   |          |      |   |     | .14 |                 |
|          |      |   |          |      |   |     | yie |                 |
|          |      |   |          |      |   |     | ld) |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| Upper    | SDG  |   | 70       | 66   | 4 |     | 0.  | Sect. 3.4-9,    |
| Support  | 3913 |   | 50-T7452 |      | 0 |     | 096 | Note 26         |
| rings    | 5786 |   | Forging  |      | . |     |     |                 |
|          |      |   |          |      | 8 |     |     |                 |
|          |      |   |          |      | 5 |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| Lower    | SEG  |   | 70       | 66   | 3 |     | 0   | Sect. 3.5-10,   |
| Support  | 3913 |   | 50-T7452 |      | 1 |     | .44 | Note 26         |
| rings    | 5785 |   | Forging  |      | . |     |     |                 |
|          |      |   |          |      | 4 |     |     |                 |
|          |      |   |          |      | 7 |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| Upper    | SDG  |   | 70       | 68   | 2 |     | 0   | Sect. 3.6-5,    |
| I/F      | 3913 |   | 50-T7451 |      | 2 |     | .96 | Note 26         |
| plate    | 5788 |   | Plate    |      | . |     |     |                 |
| assy.    |      |   |          |      | 8 |     |     |                 |
|          |      |   |          |      | 1 |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| Lower    | SDG  |   | 70       | 68   | 1 |     | 2   | Sect. 3.7-5,    |
| I/F      | 3913 |   | 50-T7451 |      | 3 |     | .36 | Note 26         |
| plate    | 5789 |   | Plate    |      | . |     |     |                 |
| assy.    |      |   |          |      | 3 |     |     |                 |
|          |      |   |          |      | 1 |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| **Margin |      |   |          |      |   |     |     |                 |
| of       |      |   |          |      |   |     |     |                 |
| Safety   |      |   |          |      |   |     |     |                 |
| Summary  |      |   |          |      |   |     |     |                 |
| of       |      |   |          |      |   |     |     |                 |
| AMS-02   |      |   |          |      |   |     |     |                 |
| USS-02   |      |   |          |      |   |     |     |                 |
| Comp     |      |   |          |      |   |     |     |                 |
| onents** |      |   |          |      |   |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| Item     | Dra  |   | Material | Mate | M |     | Mar | Comments        |
|          | wing |   | and      | rial | a |     | gin |                 |
|          | nu   |   | temper   | a    | x |     | of  |                 |
|          | mber |   |          | llow | . |     | Saf |                 |
|          |      |   |          | able | a |     | ety |                 |
|          |      |   |          | st   | p |     | (u  |                 |
|          |      |   |          | ress | p |     | lt) |                 |
|          |      |   |          | (    | l |     | FS= |                 |
|          |      |   |          | ksi) | i |     | 1.4 |                 |
|          |      |   |          |      | e |     |     |                 |
|          |      |   |          |      | d |     |     |                 |
|          |      |   |          |      | t |     |     |                 |
|          |      |   |          |      | e |     |     |                 |
|          |      |   |          |      | n |     |     |                 |
|          |      |   |          |      | s |     |     |                 |
|          |      |   |          |      | i |     |     |                 |
|          |      |   |          |      | l |     |     |                 |
|          |      |   |          |      | e |     |     |                 |
|          |      |   |          |      | s |     |     |                 |
|          |      |   |          |      | t |     |     |                 |
|          |      |   |          |      | r |     |     |                 |
|          |      |   |          |      | e |     |     |                 |
|          |      |   |          |      | s |     |     |                 |
|          |      |   |          |      | s |     |     |                 |
|          |      |   |          |      | ( |     |     |                 |
|          |      |   |          |      | k |     |     |                 |
|          |      |   |          |      | s |     |     |                 |
|          |      |   |          |      | i |     |     |                 |
|          |      |   |          |      | ) |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| Sill     | SDG  |   | Custom   | 200  | 1 |     | 0   | Sect. 2.1.5-42, |
| Trunnion | 3913 |   | 455      |      | 1 |     | .6( | Note 27         |
|          | 5732 |   | H1000    |      | 7 |     | yie |                 |
|          |      |   |          |      | . |     | ld) |                 |
|          |      |   |          |      | 5 |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| Keel     | SDG  |   | Custom   | 200  | 1 |     | 0.  | Sect. 2.3.4-12  |
| Trunnion | 3913 |   | 455      |      | 0 |     | 51( | Note 27         |
|          | 5772 |   | H1000    |      | 2 |     | yie |                 |
|          |      |   |          |      | . |     | ld) |                 |
|          |      |   |          |      | 7 |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| Upper VC | SDG  |   | 70       | 69   | 4 |     | 0   | Sect.2.1.1-10,  |
| Joint    | 3913 |   | 50-T7451 |      | 3 |     | .04 | Note 27         |
|          | 5727 |   | Plate    |      | . |     |     |                 |
|          |      |   |          |      | 8 |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| Lower VC | SDG  |   | 70       | 67   | 4 |     | 0   | Page 2.1.9-13,  |
| Joint    | 3913 |   | 50-T7451 |      | 0 |     | .06 | Note 27         |
|          | 5737 |   | Plate    |      | . |     |     |                 |
|          |      |   |          |      | 7 |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| Sill     | SDG  |   | 70       | 66   | 2 |     | 0   | page.2.1.3-10   |
| joint    | 3913 |   | 50-T7451 |      | 6 |     | .55 | Note 27         |
| primary  | 5730 |   | Plate    |      | . |     |     |                 |
| s        |      |   |          |      | 7 |     |     |                 |
| econdary |      |   |          |      |   |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| Diagonal | SEG  |   | 707      | 37   | 1 |     | 0   | Sect.           |
| strut    | 3913 |   | 5-T73511 |      | 6 |     | .58 | 2.1.13.2-5,     |
| end      | 5743 |   |          |      | . |     | (   | Note 27         |
| fitting  |      |   |          |      | 1 |     | Thr |                 |
|          |      |   |          |      | 9 |     | ead |                 |
|          |      |   |          |      |   |     | she |                 |
|          |      |   |          |      |   |     | ar) |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| Diagonal | SEG  |   | 60       | 7    | 3 |     | 0   | Sect.           |
| strut    | 3913 |   | 61-T6511 | 5.34 | 4 |     | .58 | 2.1.13.1-5,     |
| tube     | 5742 |   |          | lbf  | . |     | (   | Note 27         |
|          |      |   |          |      | 0 |     | buc |                 |
|          |      |   |          |      | 5 |     | kli |                 |
|          |      |   |          |      | l |     | ng) |                 |
|          |      |   |          |      | b |     |     |                 |
|          |      |   |          |      | f |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| Lower    | SDG  |   | 70       | 70   | 3 |     | 0   | Sect. 2.2.1-14, |
| center   | 3913 |   | 50-T7451 |      | 8 |     | .18 | Note 27         |
| body     | 5759 |   | Plate    |      | . |     |     |                 |
| joint    | SDG  |   |          |      | 8 |     |     |                 |
|          | 3913 |   |          |      |   |     |     |                 |
|          | 5760 |   |          |      |   |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| Sill     | SDG  |   | 70       | 66   | 3 |     | 0   | Sect.2.1.7-22,  |
| elbow    | 3913 |   | 50-T7451 |      | 5 |     | .21 | Note 27         |
| joint    | 5734 |   | Plate    |      | . |     |     |                 |
|          |      |   |          |      | 7 |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| Keel     | SEG  |   | 70       | 67   | 2 |     | 0   | Sect.2.3.2-13,  |
| block    | 3913 |   | 50-T7451 |      | 6 |     | .63 | Note 27         |
|          | 5770 |   | Plate    |      | . |     |     |                 |
|          |      |   |          |      | 7 |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| Diagonal | SEG  |   | 70       | 66   | 4 |     | 0   | Sect. 2.1.12-2, |
| sill     | 3913 |   | 50-T7451 |      | 2 |     | .03 | Note 27         |
| bracket  | 5740 |   | Plate    |      | . |     |     |                 |
|          |      |   |          |      | 0 |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| Sill     | SEG  |   | 70       | 66   | 3 |     | 0   | Sect. 2.1.10-8, |
| bracket  | 3913 |   | 50-T7451 |      | 1 |     | .40 | Note 27         |
|          | 5738 |   | Plate    |      | . |     |     |                 |
|          |      |   |          |      | 0 |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| Lower    | SDG  |   | 70       | 66   | 2 |     | 1   | Sect 2.2.4-16,  |
| USS to   | 3913 |   | 50-T7451 |      | 0 |     | .15 | Note 27         |
| Upper    | 5762 |   | Plate    |      | . |     |     |                 |
| USS      |      |   |          |      | 9 |     |     |                 |
| joint    |      |   |          |      |   |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| **Margin |      |   |          |      |   |     |     |                 |
| of       |      |   |          |      |   |     |     |                 |
| Safety   |      |   |          |      |   |     |     |                 |
| Summary  |      |   |          |      |   |     |     |                 |
| for      |      |   |          |      |   |     |     |                 |
| AMS-02   |      |   |          |      |   |     |     |                 |
| Payload  |      |   |          |      |   |     |     |                 |
| Attach   |      |   |          |      |   |     |     |                 |
| System   |      |   |          |      |   |     |     |                 |
| (PAS)**  |      |   |          |      |   |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| Item     | Dra  |   | Material | Mate | M |     | Mar | Comments        |
|          | wing |   | and      | rial | a |     | gin |                 |
|          |      |   | temper   | a    | x |     | of  |                 |
|          | nu   |   |          | llow | . |     | Saf |                 |
|          | mber |   |          | able | a |     | ety |                 |
|          |      |   |          | st   | p |     | (u  |                 |
|          |      |   |          | ress | p |     | lt) |                 |
|          |      |   |          | (    | l |     | FS= |                 |
|          |      |   |          | ksi) | i |     | 2.0 |                 |
|          |      |   |          |      | e |     |     |                 |
|          |      |   |          |      | d |     |     |                 |
|          |      |   |          |      | s |     |     |                 |
|          |      |   |          |      | t |     |     |                 |
|          |      |   |          |      | r |     |     |                 |
|          |      |   |          |      | e |     |     |                 |
|          |      |   |          |      | s |     |     |                 |
|          |      |   |          |      | s |     |     |                 |
|          |      |   |          |      | ( |     |     |                 |
|          |      |   |          |      | k |     |     |                 |
|          |      |   |          |      | s |     |     |                 |
|          |      |   |          |      | i |     |     |                 |
|          |      |   |          |      | ) |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| PAS      | SDG  |   | 70       | 73   | 3 |     | 0.  | Sect 4.3-6,     |
| platform | 3913 |   | 50-T7451 |      | 1 |     | 072 | Note28          |
|          | 5817 |   | Plate    |      | . |     |     |                 |
|          |      |   |          |      | 3 |     |     |                 |
|          |      |   |          |      | 3 |     |     |                 |
|          |      |   |          |      | 9 |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| Capture  | SEG  |   | A 286    | 130  | 5 |     | 0.  | Sect. 4.11.1-7, |
| bar      | 3913 |   | bar      |      | 9 |     | 052 | Note 28         |
|          | 5849 |   |          |      | . |     |     |                 |
|          |      |   |          |      | 3 |     |     |                 |
|          |      |   |          |      | 2 |     |     |                 |
|          |      |   |          |      | 1 |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| Bridge   | SDG  |   | 70       | 73   | 3 |     | 0.  | Sect 4.6-9,     |
| beam     | 3913 |   | 50-T7451 |      | 1 |     | 082 | Note 28         |
|          | 5838 |   | Plate    |      | . |     |     |                 |
|          |      |   |          |      | 0 |     |     |                 |
|          |      |   |          |      | 4 |     |     |                 |
|          |      |   |          |      | 7 |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| Bearing  | SEG  |   | 15-5-PH  | 155  | 1 |     | 0.  | Sect 4.10-8,    |
| Housing  | 3913 |   | H1025    |      | 2 |     | 236 | Note 28         |
|          | 5845 |   |          |      | 5 |     |     |                 |
|          |      |   |          |      | . |     |     |                 |
|          |      |   |          |      | 3 |     |     |                 |
|          |      |   |          |      | 8 |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| **Margin |      |   |          |      |   |     |     |                 |
| of       |      |   |          |      |   |     |     |                 |
| Safety   |      |   |          |      |   |     |     |                 |
| Summary  |      |   |          |      |   |     |     |                 |
| of       |      |   |          |      |   |     |     |                 |
| AMS-02   |      |   |          |      |   |     |     |                 |
| UPS**    |      |   |          |      |   |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| Item     | Dra  |   | Material | Mate | M |     | Mar | Comments        |
|          | wing |   | and      | rial | a |     | gin |                 |
|          | nu   |   | temper   | a    | x |     | of  |                 |
|          | mber |   |          | llow | . |     | Saf |                 |
|          |      |   |          | able | a |     | ety |                 |
|          |      |   |          | st   | p |     | (u  |                 |
|          |      |   |          | ress | p |     | lt) |                 |
|          |      |   |          | (    | l |     | FS= |                 |
|          |      |   |          | ksi) | i |     | 2.0 |                 |
|          |      |   |          |      | e |     |     |                 |
|          |      |   |          |      | d |     |     |                 |
|          |      |   |          |      | s |     |     |                 |
|          |      |   |          |      | t |     |     |                 |
|          |      |   |          |      | r |     |     |                 |
|          |      |   |          |      | e |     |     |                 |
|          |      |   |          |      | s |     |     |                 |
|          |      |   |          |      | s |     |     |                 |
|          |      |   |          |      | ( |     |     |                 |
|          |      |   |          |      | k |     |     |                 |
|          |      |   |          |      | s |     |     |                 |
|          |      |   |          |      | i |     |     |                 |
|          |      |   |          |      | ) |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| UPS Box  |      |   | 70       | 66.0 | 5 |     | 5   | Page5, 6 Note24 |
|          |      |   | 75-T7351 |      | . |     | .13 |                 |
|          |      |   |          |      | 3 |     |     |                 |
|          |      |   |          |      | 9 |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| **Margin |      |   |          |      |   |     |     |                 |
| of       |      |   |          |      |   |     |     |                 |
| Safety   |      |   |          |      |   |     |     |                 |
| Summary  |      |   |          |      |   |     |     |                 |
| of       |      |   |          |      |   |     |     |                 |
| AMS-02   |      |   |          |      |   |     |     |                 |
| E-       |      |   |          |      |   |     |     |                 |
| Crates** |      |   |          |      |   |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| Item     | Dra  |   | Material | Mate | M |     | Mar | Comments        |
|          | wing |   | and      | rial | a |     | gin |                 |
|          | num  |   | temper   | a    | x |     | of  |                 |
|          | ber  |   |          | llow | . |     | Saf |                 |
|          |      |   |          | able | a |     | ety |                 |
|          |      |   |          | st   | p |     | (u  |                 |
|          |      |   |          | ress | p |     | lt) |                 |
|          |      |   |          | (    | l |     | FS= |                 |
|          |      |   |          | ksi) | i |     | 2.0 |                 |
|          |      |   |          |      | e |     |     |                 |
|          |      |   |          |      | d |     |     |                 |
|          |      |   |          |      | s |     |     |                 |
|          |      |   |          |      | t |     |     |                 |
|          |      |   |          |      | r |     |     |                 |
|          |      |   |          |      | e |     |     |                 |
|          |      |   |          |      | s |     |     |                 |
|          |      |   |          |      | s |     |     |                 |
|          |      |   |          |      | ( |     |     |                 |
|          |      |   |          |      | k |     |     |                 |
|          |      |   |          |      | s |     |     |                 |
|          |      |   |          |      | i |     |     |                 |
|          |      |   |          |      | ) |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| Bottom   |      |   | 70       | 62.9 | 1 |     | 1   | Page 50, Note   |
| plate    |      |   | 75-T7351 |      | 3 |     | .34 | 25              |
|          |      |   |          |      | . |     |     |                 |
|          |      |   |          |      | 5 |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| Lateral  |      |   | 70       | 62.9 | 8 |     | 2   | Page 50, Note   |
| wall     |      |   | 75-T7351 |      | . |     | .53 | 25              |
|          |      |   |          |      | 9 |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| **Margin |      |   |          |      |   |     |     |                 |
| of       |      |   |          |      |   |     |     |                 |
| Safety   |      |   |          |      |   |     |     |                 |
| Summary  |      |   |          |      |   |     |     |                 |
| of       |      |   |          |      |   |     |     |                 |
| Cr       |      |   |          |      |   |     |     |                 |
| yomagnet |      |   |          |      |   |     |     |                 |
| Avionics |      |   |          |      |   |     |     |                 |
| Box**    |      |   |          |      |   |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| Item     | Dra  |   | Material | Mate | M |     | Mar | Comments        |
|          | wing |   | and      | rial | a |     | gin |                 |
|          | num  |   | temper   | a    | x |     | of  |                 |
|          | ber  |   |          | llow | . |     | Saf |                 |
|          |      |   |          | able | a |     | ety |                 |
|          |      |   |          | st   | p |     | (u  |                 |
|          |      |   |          | ress | p |     | lt) |                 |
|          |      |   |          | (    | l |     | FS= |                 |
|          |      |   |          | ksi) | i |     | 2.0 |                 |
|          |      |   |          |      | e |     |     |                 |
|          |      |   |          |      | d |     |     |                 |
|          |      |   |          |      | s |     |     |                 |
|          |      |   |          |      | t |     |     |                 |
|          |      |   |          |      | r |     |     |                 |
|          |      |   |          |      | e |     |     |                 |
|          |      |   |          |      | s |     |     |                 |
|          |      |   |          |      | s |     |     |                 |
|          |      |   |          |      | ( |     |     |                 |
|          |      |   |          |      | k |     |     |                 |
|          |      |   |          |      | s |     |     |                 |
|          |      |   |          |      | i |     |     |                 |
|          |      |   |          |      | ) |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+
| Base     | AM   |   | 6061-T6  | 42.0 | 3 |     | 5   | Page 34, Note   |
| plate    | S-AD |   |          |      | . |     |     | 29              |
|          | -CAB |   |          |      | 7 |     |     |                 |
|          |      |   |          |      | 9 |     |     |                 |
|          | 0    |   |          |      |   |     |     |                 |
|          | 0000 |   |          |      |   |     |     |                 |
|          | -CRS |   |          |      |   |     |     |                 |
+----------+------+---+----------+------+---+-----+-----+-----------------+

NOTE:

1\) Ref. Transition Radiation Detector (TRD), Structural Verification
Presentation, Rev.3, 11 April 2005

2\) Ref. TRD Gas System Box S Mechanical structure AMS-02, Rev_1, 27
June 2005, INFN Rome and MIT

3\) Ref. TRD Box C Finite element analysis, MIT \@CERN, June 11, 2004

4\) Ref. Upper Time of Flight structural Analysis Report,
RICSYS-CGS-013, issue 1, 29 June 2004

5\) Tsai-Hill equation shown in Ref. note 4, Page 38. Margin of safety
is (1/ Failure Index)-1

6\) Ref. Lower Time of flight (LTOF) structural Analysis Report,
RICSYS-RP_CGS-012 issue1, 29 June 2004

7\) Tsai-Hill equation shown in Ref. note 6, page 44. Margin of safety
is (1/ Failure index)-1.

8\) Ref. RICH Structural Analysis report, RICSYS-RP-CGS-009, issue1, 29
June 2004

9\) Tsai-Hill equation shown in Ref. note 8 page 44. Margin of safety =
(1/ Failure index)-1

10\) Ref. Flight ECAL Stress analysis after weight saving, 7 April 2004

11\) Ref. AMS-02 AMICA Star Tracker Support Design, Rev. 1 INFN Rome, 27
June 2005

11a) Tsai-Hill equation shown in report note 11 page 12. Margin of
safety = (1/FSult Failure index)-1

12\) Ref. Baffle Support design, INFN Rome, Rev1 27 June 2005

13\) Ref. AMS Silicon Tracker Support Plates Analysis Report Extension
AMS-ANR-002, Contraves Space, 19 November 1999.

14\) Ref. AMS 02 Tracker Support Feet, Rev. 1 Structural Verification
Document, ISATEC, 16 June 2004

15\) Reference summary of Structural Analysis of AMS-02 Super conducting
Magnet, September 2003, issue 02

16\) Ref. Helium tank Strength assessment, October 24, 2006

17\) Ref. Cryomagnet Suspension Strap Analysis, Lockheed Martin, April
2002

18\) Ref. Space Cryomagnetics Ltd (SCL) analysis, Fax No.1169, 6 March
2002

19\) Ref. AMS-02 Anti Coincidence Counter Structural Verification
Document, Rev. 1, ISATEC, 9 Dec. 2004

20\) Ref. Zenith Radiator Structural analysis Report, AMS-OHB-SAR-001,
issue 4, April. 1, 2005

21\) \<Deleted\>

22\) Ref. Main Radiator Structural analysis Report, AMS-02-RP-CGS-005,
issue 4, April 5, 2007

23\) Ref. HV Bricks Structural analysis Report, AMS-02-RP-CGS-007, issue
1, November.22, 2004

24\) Ref. UPS Box Redesign Structural Analysis Report, CSIST Taiwan,
December 28, 2005

25\) Ref. Report AMS-02 RP-CGS-003, issue 2, Carlo Gavazzi Space, 4
August 2005

26\) Ref. AMS-02, Strength and Stability of Vacuum Case Assembly report

27\) Ref. AMS-02, Strength and Stability for USS-02 report

28\) Ref. AMS-02 PAS analysis report

29\) Ref. Cryomagnet Avionics Box Mechanical Analysis, CAB-AN-CRS-0055,
issue 2, September 22, 2006, EADS

ASTRIUM, CRISA

30\) Ref. Transition Radiation Detector (TRD), Structural Verification
Presentation, Rev.5, 7 March 2007

31\) Ref. ACC Connector Support, Documentation of Margin of Safety, 8
March 2007

**AMS-02 FASTENERS MARGIN OF SAFETY**

+----------+-------+--------+----+--------+-------+----------------+
| TRD      |       |        |    |        |       |                |
| F        |       |        |    |        |       |                |
| asteners |       |        |    |        |       |                |
+----------+-------+--------+----+--------+-------+----------------+
| Item     | Dr    | Ma     | Ma | A      | M     | Comments       |
|          | awing | terial | te | pplied | argin |                |
|          | n     | and    | ri | Load   | of    |                |
|          | umber | temper | al | (lbf)  | S     |                |
|          |       |        | a  |        | afety |                |
|          |       |        | ll |        | (ult) |                |
|          |       |        | ow |        | F     |                |
|          |       |        | ab |        | S=2.0 |                |
|          |       |        | le |        |       |                |
|          |       |        | st |        |       |                |
|          |       |        | re |        |       |                |
|          |       |        | ss |        |       |                |
|          |       |        | (  |        |       |                |
|          |       |        | ks |        |       |                |
|          |       |        | i) |        |       |                |
+----------+-------+--------+----+--------+-------+----------------+
| Corner   | S     | NA     | 1  | T      | 0.095 | Total tension  |
| bracket  | EG391 | S1958C | 80 | ension |       | yield,         |
| to upper | 35720 |        |    | = 2295 |       | 2.4.1.3-13,    |
| VC joint |       | 0.     |    |        |       |                |
|          |       | 50-20, |    | Shear  |       | Note 10        |
|          |       | A286   |    | = 1130 |       |                |
+----------+-------+--------+----+--------+-------+----------------+
| Upper    |       | 1      | 1  | T      | 0.02  | Joint          |
| bracket  |       | /4-28, | 60 | ension |       | separation,    |
| to M     |       | A286   |    | = 1167 |       | Note 1, Load   |
| s        |       |        |    |        |       | case 1008      |
| tructure |       |        |    | Shear  |       |                |
|          |       |        |    | = 0    |       |                |
+----------+-------+--------+----+--------+-------+----------------+
| Corner   |       | 5/     | 2  | T      | 0.04  | Joint          |
| bracket  |       | 16-24, | 00 | ension |       | separation,    |
| to M     |       | A286   |    | = 2656 |       | Note 1, Load   |
| s        |       |        |    |        |       | case 4058      |
| tructure |       |        |    | Shear  |       |                |
|          |       |        |    | = 84   |       |                |
+----------+-------+--------+----+--------+-------+----------------+
| Upper    |       | 1      | 1  | T      | 0.01  | Total tension  |
| brackets |       | /4-28, | 40 | ension |       | yield, Note 1, |
| to upper |       | A286   |    | = 900  |       | Load case 1008 |
| cover    |       |        |    |        |       |                |
|          |       |        |    | Shear  |       |                |
|          |       |        |    | = 6    |       |                |
+----------+-------+--------+----+--------+-------+----------------+
| Upper    |       | 5/     | 1  | T      | 0.08  | Total tension  |
| cover to |       | 16-24, | 40 | ension |       | yield, Note 1, |
| octagon  |       | A286   |    | = 155  |       | Load case 1008 |
|          |       |        |    |        |       |                |
|          |       |        |    | Shear  |       |                |
|          |       |        |    | = 237  |       |                |
+----------+-------+--------+----+--------+-------+----------------+
| TRD Gas  |       |        |    |        |       |                |
| System   |       |        |    |        |       |                |
| F        |       |        |    |        |       |                |
| asteners |       |        |    |        |       |                |
+----------+-------+--------+----+--------+-------+----------------+
| Item     | Dr    | Ma     |    | A      | M     | Comments       |
|          | awing | terial | Ma | pplied | argin |                |
|          | n     | and    | te | Load   | of    |                |
|          | umber | temper | ri | (lbf)  | S     |                |
|          |       |        | al |        | afety |                |
|          |       |        | a  |        | (ult) |                |
|          |       |        | ll |        | F     |                |
|          |       |        | ow |        | S=2.0 |                |
|          |       |        | ab |        |       |                |
|          |       |        | le |        |       |                |
|          |       |        | st |        |       |                |
|          |       |        | re |        |       |                |
|          |       |        | ss |        |       |                |
|          |       |        | (  |        |       |                |
|          |       |        | ks |        |       |                |
|          |       |        | i) |        |       |                |
+----------+-------+--------+----+--------+-------+----------------+
| Box      |       | N      | 1  | T      | 0.01  | Total tension  |
| S/BoxC   |       | AS1954 | 80 | ension |       | yield, Note 2  |
| plate to |       | 0      |    | = 148  |       | page 13        |
| USS      |       | .25-28 |    |        |       |                |
| upper    |       | A-286  |    | Shear  |       |                |
| I/F      |       |        |    | = 978  |       |                |
| bolts    |       |        |    |        |       |                |
+----------+-------+--------+----+--------+-------+----------------+
| Box S Xe |       | NA     | 1  | T      | 0.01  | Total tension  |
| bracket  |       | S1351N | 60 | ension |       | yield, Note 2, |
| to plate |       | 0.     |    | = 816  |       | page 19        |
| bolts    |       | 375-24 |    |        |       |                |
|          |       | A-286  |    | Shear  |       |                |
|          |       |        |    | = 698  |       |                |
+----------+-------+--------+----+--------+-------+----------------+
| Box C    |       | NA     | 1  | T      | 0.04  | Total tension  |
| mounting |       | S1351N | 60 | ension |       | yield, Note 3, |
| of       |       | 0.1    |    | = 24   |       | Page 5         |
| cylinder |       | 90-32, |    |        |       |                |
| to       |       | A-286  |    | Shear  |       |                |
| bracket  |       |        |    | = 48   |       |                |
+----------+-------+--------+----+--------+-------+----------------+
| Box C    |       | NA     | 1  | T      | 0.01  | Total tension  |
| mounting |       | S135N1 | 60 | ension |       | yield , Note   |
| of valve |       | 0.1    |    | = 44   |       | 3,             |
| bracket  |       | 90-32, |    |        |       |                |
| to       |       | A-286  |    | Shear  |       | Page 12        |
| holder   |       |        |    | = 85   |       |                |
+----------+-------+--------+----+--------+-------+----------------+
| AMS-02   |       |        |    |        |       |                |
| Upper    |       |        |    |        |       |                |
| Time of  |       |        |    |        |       |                |
| Flight   |       |        |    |        |       |                |
| (UTOF)   |       |        |    |        |       |                |
| F        |       |        |    |        |       |                |
| asteners |       |        |    |        |       |                |
+----------+-------+--------+----+--------+-------+----------------+
| Item     | Dr    | Ma     |    | A      | M     | Comments       |
|          | awing | terial | Ma | pplied | argin |                |
|          | n     | and    | te | Load   | of    |                |
|          | umber | temper | ri | (lbf)  | S     |                |
|          |       |        | al |        | afety |                |
|          |       |        | a  |        | (ult) |                |
|          |       |        | ll |        | F     |                |
|          |       |        | ow |        | S=2.0 |                |
|          |       |        | ab |        |       |                |
|          |       |        | le |        |       |                |
|          |       |        | st |        |       |                |
|          |       |        | re |        |       |                |
|          |       |        | ss |        |       |                |
|          |       |        | (  |        |       |                |
|          |       |        | ks |        |       |                |
|          |       |        | i) |        |       |                |
+----------+-------+--------+----+--------+-------+----------------+
| USS I/F  | Joint | A-286, | 2  | T      | 0.10  | Total tension  |
| bolts    | 1     | 0.3    | 00 | ension |       | yield , Note 4 |
|          |       | 125-24 |    | = 2646 |       |                |
|          |       | EWB-   |    |        |       |                |
|          |       | 0420-5 |    | Shear  |       |                |
|          |       |        |    | = 0    |       |                |
+----------+-------+--------+----+--------+-------+----------------+
| Bracket  | Joint | A-286, | 1  | T      | 0.04  | Combined       |
| e        | 3     | NAS    | 60 | ension |       | tension and    |
| xtension |       | 1351N4 |    | = 465  |       |                |
| bolts    |       |        |    |        |       | Shear, Note 4  |
|          |       | 0.     |    | Shear  |       |                |
|          |       | 25-28, |    | = 961  |       |                |
+----------+-------+--------+----+--------+-------+----------------+
| Upper to | Joint | A-286, | 1  | T      | 0.16  | Total tension  |
| lower    | 4     | NAS1   | 60 | ension |       | yield , Note 4 |
| bolts    |       | 351N4, |    | = 337  |       |                |
|          |       |        |    |        |       |                |
|          |       | 0      |    | Shear  |       |                |
|          |       | .25-28 |    | = 232  |       |                |
+----------+-------+--------+----+--------+-------+----------------+
| AMS-02   |       |        |    |        |       |                |
| Lower    |       |        |    |        |       |                |
| Time of  |       |        |    |        |       |                |
| Flight   |       |        |    |        |       |                |
| (LTOF)F  |       |        |    |        |       |                |
| asteners |       |        |    |        |       |                |
+----------+-------+--------+----+--------+-------+----------------+
| Item     | Dr    | Ma     |    | A      | M     | Comments       |
|          | awing | terial | Ma | pplied | argin |                |
|          | n     | and    | te | Load   | of    |                |
|          | umber | temper | ri | (lbf)  | S     |                |
|          |       |        | al |        | afety |                |
|          |       |        | a  |        | (ult) |                |
|          |       |        | ll |        | F     |                |
|          |       |        | ow |        | S=2.0 |                |
|          |       |        | ab |        |       |                |
|          |       |        | le |        |       |                |
|          |       |        | st |        |       |                |
|          |       |        | re |        |       |                |
|          |       |        | ss |        |       |                |
|          |       |        | (  |        |       |                |
|          |       |        | ks |        |       |                |
|          |       |        | i) |        |       |                |
+----------+-------+--------+----+--------+-------+----------------+
| Bracket  | Joint | A-286, | 1  | Axial  | 0.01  | Combined       |
| to ring  | 1     | NAS    | 60 | = 633  |       | tension and    |
| bolts    |       | 1351N5 |    |        |       |                |
|          |       | 0.3    |    | Shear  |       | Shear, Note 4  |
|          |       | 125-24 |    | = 1179 |       |                |
+----------+-------+--------+----+--------+-------+----------------+
| USS to   | Joint | A-286, | 1  | Axial  | 0.03  | Joint          |
| Upper    | 2     | NAS    | 60 | = 2788 |       | separation ,   |
| bracket  |       | 1351N6 |    |        |       | Note 4         |
| bolts    |       | 0.     |    | Shear  |       |                |
|          |       | 375-24 |    | = 107  |       |                |
+----------+-------+--------+----+--------+-------+----------------+
| USS to   | Joint | A-286, | 1  | Axial  | 0.15  | Total tension  |
| Lower    | 3     | NAS    | 60 | = 108  |       | yield, Note 4  |
| bracket  |       | 1351N3 |    |        |       |                |
| bolts    |       | 0.     |    | Shear  |       |                |
|          |       | 190-32 |    | = 158  |       |                |
+----------+-------+--------+----+--------+-------+----------------+
| Ring to  | Joint | A-286, | 1  | Axial  | 0.16  | Total tension  |
| H        | 4     | NAS    | 60 | = 130  |       | yield, Note 4  |
| oneycomb |       | 1351N4 |    |        |       |                |
| bolts    |       |        |    | Shear  |       |                |
|          |       | 0      |    | = 283  |       |                |
|          |       | .25-28 |    |        |       |                |
+----------+-------+--------+----+--------+-------+----------------+
| Rod end  | Joint | NAS    | 1  | Axial  | 0.07  | Combined       |
|          | 6     | 6706   | 60 | = 0    |       | tension and    |
|          |       | DU     |    |        |       |                |
|          |       |        |    | Shear  |       | Shear, Note 4  |
|          |       | 0.     |    | = 2280 |       |                |
|          |       | 375-24 |    |        |       |                |
+----------+-------+--------+----+--------+-------+----------------+
| AMS-02   |       |        |    |        |       |                |
| Ring     |       |        |    |        |       |                |
| Imaging  |       |        |    |        |       |                |
| Chernkov |       |        |    |        |       |                |
| Counter  |       |        |    |        |       |                |
| (RICH)   |       |        |    |        |       |                |
| F        |       |        |    |        |       |                |
| asteners |       |        |    |        |       |                |
+----------+-------+--------+----+--------+-------+----------------+
| Item     | Dr    | Ma     |    | A      | M     | Comments       |
|          | awing | terial | Ma | pplied | argin |                |
|          | n     | and    | te | Load   | of    |                |
|          | umber | temper | ri | (lbf)  | S     |                |
|          |       |        | al |        | afety |                |
|          |       |        | a  |        | (ult) |                |
|          |       |        | ll |        | F     |                |
|          |       |        | ow |        | S=2.0 |                |
|          |       |        | ab |        |       |                |
|          |       |        | le |        |       |                |
|          |       |        | st |        |       |                |
|          |       |        | re |        |       |                |
|          |       |        | ss |        |       |                |
|          |       |        | (  |        |       |                |
|          |       |        | ks |        |       |                |
|          |       |        | i) |        |       |                |
+----------+-------+--------+----+--------+-------+----------------+
| External | Joint | A-286, | 1  | T      | 0.05  | Combined       |
| S        | 1     | NAS    | 60 | ension |       | tension and    |
| tructure |       | 1351N4 |    | = 84   |       |                |
| bolts    |       |        |    |        |       | Shear, Note 4  |
|          |       | 0      |    | Shear  |       |                |
|          |       | .25-28 |    | = 987  |       |                |
+----------+-------+--------+----+--------+-------+----------------+
| External | Joint | A4-70  | 1  | T      | 0.10  | Total tension  |
| to       | 2     | 0.     | 16 | ension |       | yield, Note 4  |
| Internal |       | 118-44 |    | = 89   |       |                |
| s        |       |        |    |        |       |                |
| tructure |       | (3 mm) |    | Shear  |       |                |
| bolts    |       |        |    | = 61   |       |                |
+----------+-------+--------+----+--------+-------+----------------+
| External | Joint | A-286, | 1  | T      | 0.06  | Combined       |
| S        | 3     | NAS    | 60 | ension |       | tension and    |
| tructure |       | 1351N5 |    | = 132  |       |                |
| bolts    |       | 0.3    |    |        |       | Shear, Note 4  |
|          |       | 125-24 |    | Shear  |       |                |
|          |       |        |    | = 855  |       |                |
+----------+-------+--------+----+--------+-------+----------------+
| AMS-02   |       |        |    |        |       |                |
| Electro  |       |        |    |        |       |                |
| Magnetic |       |        |    |        |       |                |
| Cal      |       |        |    |        |       |                |
| orimeter |       |        |    |        |       |                |
| (ECAL)   |       |        |    |        |       |                |
| F        |       |        |    |        |       |                |
| asteners |       |        |    |        |       |                |
+----------+-------+--------+----+--------+-------+----------------+
| Item     | Dr    | Ma     |    | A      | M     | Comments       |
|          | awing | terial | Ma | pplied | argin |                |
|          | n     | and    | te | Load   | of    |                |
|          | umber | temper | ri | (lbf)  | S     |                |
|          |       |        | al |        | afety |                |
|          |       |        | a  |        | (ult) |                |
|          |       |        | ll |        | F     |                |
|          |       |        | ow |        | S=1.4 |                |
|          |       |        | ab |        |       |                |
|          |       |        | le |        |       |                |
|          |       |        | st |        |       |                |
|          |       |        | re |        |       |                |
|          |       |        | ss |        |       |                |
|          |       |        | (  |        |       |                |
|          |       |        | ks |        |       |                |
|          |       |        | i) |        |       |                |
+----------+-------+--------+----+--------+-------+----------------+
| Support  | ECA   | A-286  | 1  | T      | 0.081 | Total tension  |
| beam to  | L0-0E | 0.3    | 60 | ensile |       | yield,         |
| bracket  |       | 125-24 |    | = 2728 |       | Negative MS    |
| (Joint   |       | NAS    |    |        |       | for Joint      |
| 1)       |       | 6      |    | Shear  |       | separation,    |
|          |       | 705U7, |    | =0.0   |       | Note 8         |
|          |       | 8      |    |        |       |                |
+----------+-------+--------+----+--------+-------+----------------+
| Bracket  | ECA   | A-286  | 1  | T      | 0.042 | Total tension  |
| to side  | L0-0E | 0      | 80 | ensile |       | yield,         |
| panels   |       | .25-28 |    | = 3201 |       | Negative MS    |
| (joint   |       | NAS    |    |        |       | for Joint      |
| 2)       |       | 1954C6 |    | Shear  |       | separation,    |
|          |       |        |    | = 264  |       | Note 8         |
+----------+-------+--------+----+--------+-------+----------------+
| I Frame  | ECA   | A-286  | 1  | T      | 0.20  | Total tension  |
| to       | L0-0E | 0.3    | 60 | ensile |       | yield, Note 8  |
| bracket  |       | 125-24 |    | = 358  |       |                |
| bolts    |       | NAS    |    |        |       |                |
| (joint   |       | 67     |    | Shear  |       |                |
| 3)       |       | 05HU10 |    | = 0.0  |       |                |
+----------+-------+--------+----+--------+-------+----------------+
| I Frame  | ECA   | A-286  | 1  | T      | 0.08  | Combined       |
| to       | L0-0E | 0      | 40 | ensile |       | tension and    |
| h        |       | .25-28 |    | = 156  |       | shear, Note 8  |
| oneycomb |       | NAS    |    |        |       |                |
| rei      |       | 1004-2 |    | Shear  |       |                |
| nforcing |       |        |    | = 1287 |       |                |
| and side |       |        |    |        |       |                |
| panels 1 |       |        |    |        |       |                |
| and 2    |       |        |    |        |       |                |
| bolts    |       |        |    |        |       |                |
| (joint4) |       |        |    |        |       |                |
+----------+-------+--------+----+--------+-------+----------------+
| I Frame  | ECA   | A-286  | 1  |        |       | Bolts were     |
| to side  | L0-0E | 0      | 40 |        |       | overtorqued.   |
| panel 1  |       | .25-28 |    |        |       | This joint is  |
| bol      |       | NAS    |    |        |       | removed from   |
| ts(Joint |       | 1004-9 |    |        |       | model to       |
| 5)       |       |        |    |        |       | re-evaluate    |
|          |       |        |    |        |       | bolt loads     |
+----------+-------+--------+----+--------+-------+----------------+
| I-Frame  | ECA   | A-286  | 1  | T      | 0.165 | Total tension  |
| to side  | L0-0E | 0.3    | 40 | ensile |       | yield, Note 8  |
| panels 1 |       | 125-24 |    | = 335  |       |                |
| and 2    |       |        |    |        |       |                |
| (joint   |       | NAS100 |    | Shear  |       |                |
| 6)       |       | 5-1,-2 |    | = 563  |       |                |
+----------+-------+--------+----+--------+-------+----------------+
| I-Frame  | ECA   | A-286  | 1  | T      | 0.141 | Total tension  |
| to       | L0-0E | 0.3    | 40 | ensile |       | yield, Note 8  |
| h        |       | 125-24 |    | = 887  |       |                |
| oneycomb |       |        |    |        |       |                |
| rei      |       | NAS    |    | Shear  |       |                |
| nforcing |       | 1005-1 |    | = 601  |       |                |
| and side |       |        |    |        |       |                |
| panels 1 |       |        |    |        |       |                |
| and 2    |       |        |    |        |       |                |
|          |       |        |    |        |       |                |
| (Joint   |       |        |    |        |       |                |
| 7)       |       |        |    |        |       |                |
+----------+-------+--------+----+--------+-------+----------------+
| Support  | ECA   | A-286  | 1  | T      | 0.171 | Total Tension  |
| beam to  | L0-0E | 0.     | 40 | ensile |       | yield, Note 8  |
| USS      |       | 625-18 |    | = 4389 |       |                |
|          |       | NAS    |    |        |       |                |
| (Joint   |       | 1      |    | Shear  |       |                |
| 8)       |       | 960C30 |    | = 1270 |       |                |
+----------+-------+--------+----+--------+-------+----------------+
| AMS-02   |       |        |    |        |       |                |
| Star     |       |        |    |        |       |                |
| Tracker  |       |        |    |        |       |                |
| F        |       |        |    |        |       |                |
| asteners |       |        |    |        |       |                |
+----------+-------+--------+----+--------+-------+----------------+
| Item     | Dr    | Ma     |    | A      | M     | Comments       |
|          | awing | terial | Ma | pplied | argin |                |
|          | n     | and    | te | Load   | of    |                |
|          | umber | temper | ri | (lbf)  | S     |                |
|          |       |        | al |        | afety |                |
|          |       |        | a  |        | (ult) |                |
|          |       |        | ll |        | F     |                |
|          |       |        | ow |        | S=2.0 |                |
|          |       |        | ab |        |       |                |
|          |       |        | le |        |       |                |
|          |       |        | st |        |       |                |
|          |       |        | re |        |       |                |
|          |       |        | ss |        |       |                |
|          |       |        | (  |        |       |                |
|          |       |        | ks |        |       |                |
|          |       |        | i) |        |       |                |
+----------+-------+--------+----+--------+-------+----------------+
| Upper    |       | A286,  | 1  | T      | 0.005 | Total tension  |
| bracket  |       | 0.39   | 60 | ension |       | Yield, Note 5, |
| to       |       | (M10)  |    | = 67   |       | page V         |
| tracker  |       |        |    |        |       |                |
| plane 1  |       |        |    | Shear  |       |                |
| bolts    |       |        |    | = 268  |       |                |
+----------+-------+--------+----+--------+-------+----------------+
| Upper    |       | A286,  | 1  | T      | 0.009 | Total tension  |
| bracket  |       | 0.     | 60 | ension |       | Yield , Note   |
| to lower |       | 190-32 |    | = 125  |       | 5,             |
| bracket  |       |        |    |        |       |                |
| bolts    |       |        |    | Shear  |       | Page IX        |
|          |       |        |    | =116   |       |                |
+----------+-------+--------+----+--------+-------+----------------+
| Lower    |       | A286,  | 1  | T      | 0.03  | Total tension  |
| bracket  |       | 0.118  | 60 | ension |       | Yield, Note 5. |
| to       |       | (M3)   |    | = 8    |       | page XIII      |
| tracker  |       |        |    |        |       |                |
| conical  |       |        |    | Shear  |       |                |
| flange   |       |        |    | = 112  |       |                |
+----------+-------+--------+----+--------+-------+----------------+
| Baffle   |       | A286   | 1  | T      | 0.03  | Total tension  |
| bracket  |       | 0.     | 60 | ension |       | Yield, Note 6, |
| Baffle   |       | 190-32 |    | = 38   |       | page XIV       |
| side to  |       |        |    |        |       |                |
| Baffle   |       |        |    | Shear  |       |                |
| bolts    |       |        |    | = 14   |       |                |
+----------+-------+--------+----+--------+-------+----------------+
| AMS-02   |       |        |    |        |       |                |
| Silicon  |       |        |    |        |       |                |
| Tracker  |       |        |    |        |       |                |
| S        |       |        |    |        |       |                |
| tructure |       |        |    |        |       |                |
| F        |       |        |    |        |       |                |
| asteners |       |        |    |        |       |                |
+----------+-------+--------+----+--------+-------+----------------+
| Item     | Dr    | Ma     |    | A      | M     | Comments       |
|          | awing | terial | Ma | pplied | argin |                |
|          | n     | and    | te | Load   | of    |                |
|          | umber | temper | ri | (lbf)  | S     |                |
|          |       |        | al |        | afety |                |
|          |       |        | a  |        | (ult) |                |
|          |       |        | ll |        | F     |                |
|          |       |        | ow |        | S=2.0 |                |
|          |       |        | ab |        |       |                |
|          |       |        | le |        |       |                |
|          |       |        | st |        |       |                |
|          |       |        | re |        |       |                |
|          |       |        | ss |        |       |                |
|          |       |        | (  |        |       |                |
|          |       |        | ks |        |       |                |
|          |       |        | i) |        |       |                |
+----------+-------+--------+----+--------+-------+----------------+
| Tracker  |       | A4-70, | 1  | T      | 0.02  | Joint          |
| feet to  |       | 0.3    | 01 | ension |       | separation,    |
| vacuum   |       | 125-24 | .5 | = 1072 |       | Note 17,       |
| case     |       | UNF    |    |        |       |                |
| (Joint1) |       |        |    | Shear  |       | page 2.1-4     |
|          |       |        |    | = 0    |       |                |
+----------+-------+--------+----+--------+-------+----------------+
| Tracker  |       | A-286  | 2  | T      | 0.03  | Total tension  |
| feet to  |       | 10-32  | 00 | ension |       | yield,         |
| Tracker  |       | UNF    |    | = 1196 |       | Negative MS on |
| shell    |       |        |    |        |       | Joint          |
| (Joint2) |       |        |    | Shear  |       | separation,    |
|          |       |        |    | = 0    |       | Note 17,       |
|          |       |        |    |        |       |                |
|          |       |        |    |        |       | page 2.2-4     |
+----------+-------+--------+----+--------+-------+----------------+
| Conical  |       | A-286, | 2  | T      | 0.01  | Combined       |
| Flange   |       | M4x33  | 00 | ension |       | tension and    |
| to       |       |        |    | = 327  |       | shear, Note    |
| tracker  |       |        |    |        |       | 17, page 2.3-4 |
| shell    |       |        |    | Shear  |       |                |
| (Joint3) |       |        |    | = 333  |       |                |
+----------+-------+--------+----+--------+-------+----------------+
| Tracker  |       | A4-70  | 1  | T      | 0.07  | Total tension  |
| shell to |       | 0.     | 01 | ension |       | yield, Note    |
| tracker  |       | 138-32 | .5 | = 59   |       | 17,            |
| shell    |       | UNC    |    |        |       |                |
| (Joint   |       |        |    | Shear  |       | page 2.4-4     |
| 4)       |       |        |    | = 0    |       |                |
+----------+-------+--------+----+--------+-------+----------------+
| Inner    |       | A4-70, | 1  | T      | 0.08  | Total thread   |
| plane to |       | M4x12  | 01 | ension |       | shear          |
| tracker  |       |        | .5 | = 49   |       | ultimate,      |
| shell    |       |        |    |        |       |                |
| (Joint   |       |        |    | Shear  |       | Note 17, page  |
| 5)       |       |        |    | = 60   |       | 2.5-4          |
+----------+-------+--------+----+--------+-------+----------------+
| Outer    |       | A4-70, | 1  | T      | 0.16  | Total thread   |
| plane to |       | M4x40  | 01 | ension |       | shear          |
| conical  |       |        | .5 | = 29   |       | ultimate,      |
| flange,  |       |        |    |        |       |                |
| long     |       |        |    | Shear  |       | Note 17, page  |
| flange   |       |        |    | = 80   |       | 2.6-4          |
| (Joint   |       |        |    |        |       |                |
| 6)       |       |        |    |        |       |                |
+----------+-------+--------+----+--------+-------+----------------+
| Outer    |       | A4-70, | 1  | T      | 0.05  | Total thread   |
| plane to |       | M4x40  | 01 | ension |       | shear          |
| conical  |       |        | .5 | = 29   |       | ultimate,      |
| flange,  |       |        |    |        |       |                |
| short    |       |        |    | Shear  |       | Note 17, page  |
| flange   |       |        |    | = 80   |       | 2.7-4          |
| (Joint   |       |        |    |        |       |                |
| 7)       |       |        |    |        |       |                |
+----------+-------+--------+----+--------+-------+----------------+
| F        |       |        |    |        |       |                |
| asteners |       |        |    |        |       |                |
| AMS-02   |       |        |    |        |       |                |
| Cr       |       |        |    |        |       |                |
| yomagnet |       |        |    |        |       |                |
+----------+-------+--------+----+--------+-------+----------------+
| Item     | Dr    | Ma     | Ma | A      | M     | Comments       |
|          | awing | terial | te | pplied | argin |                |
|          | N     | and    | ri | Load   | of    |                |
|          | umber | temper | al | (lbf)  | S     |                |
|          |       |        | a  |        | afety |                |
|          |       |        | ll |        | SF    |                |
|          |       |        | ow |        | =2.0  |                |
|          |       |        | ab |        |       |                |
|          |       |        | le |        |       |                |
|          |       |        | Lo |        |       |                |
|          |       |        | ad |        |       |                |
|          |       |        | (  |        |       |                |
|          |       |        | lb |        |       |                |
|          |       |        | f) |        |       |                |
+----------+-------+--------+----+--------+-------+----------------+
| RT1 to   | SC    | A4/70, | 37 | 2534   | 0.46  | Page 2,        |
| RT3      | D0831 | M8 316 | 02 |        | yield | Appendix 5     |
| bolts    |       | sta    |    |        |       | Note 7         |
|          |       | inless |    |        |       |                |
|          |       | steel  |    |        |       |                |
+----------+-------+--------+----+--------+-------+----------------+
| RT3 to   | SC    | A4/70, | 85 | 5666   | 0.50  | Page 2,        |
| RT5      | D0835 | M12    | 27 |        | yield | Appendix 5     |
| bolts    |       | 316    |    |        |       | Note 7         |
|          |       | sta    |    |        |       |                |
|          |       | inless |    |        |       |                |
|          |       | steel  |    |        |       |                |
+----------+-------+--------+----+--------+-------+----------------+
| RTEF to  | SC    | M8,    | 61 | 2468   | 1.48  | Page 2,        |
| RT5      | D0837 | 316 Hi | 29 |        | yield | Appendix 5     |
| bolts    |       | proof  |    |        |       | Note 7         |
|          |       | sta    |    |        |       |                |
|          |       | inless |    |        |       |                |
|          |       | steel  |    |        |       |                |
+----------+-------+--------+----+--------+-------+----------------+
| Dipole   | SC    | UNF    | 1  | 3758   | 3.63  | Page 2,        |
| c        | D0815 | 316 Hi | 74 |        | yield | Appendix 5     |
| rossbeam |       | proof  | 17 |        |       | Note 7         |
| to RTEF  |       | sta    |    |        |       |                |
| bolts    |       | inless |    |        |       |                |
|          |       | steel  |    |        |       |                |
+----------+-------+--------+----+--------+-------+----------------+
| Dipole   | SC    | M5,    | 23 | 1114   | 1.14  | Page 2,        |
| island   | D0824 | 316 Hi | 78 |        | yield | Appendix 5     |
| to RTEF  |       | proof  |    |        |       | Note 7         |
| bolts    |       | sta    |    |        |       |                |
|          |       | inless |    |        |       |                |
|          |       | steel  |    |        |       |                |
+----------+-------+--------+----+--------+-------+----------------+
| Dipole   | SC    | M5,    | 23 | 1166   | 1.04  | Page 2,        |
| edge     | D0824 | 316 Hi | 78 |        | yield | Appendix 5     |
| plate to |       | proof  |    |        |       | Note 7         |
| RTEF     |       | sta    |    |        |       |                |
| bolts    |       | inless |    |        |       |                |
|          |       | steel  |    |        |       |                |
+----------+-------+--------+----+--------+-------+----------------+
| Helium   | SC    | M8,    | 61 | 3313   | 0.85  | Page 2,        |
| vessel   | D0898 | 316 Hi | 29 |        | yield | Appendix 5     |
| Fz       |       | proof  |    |        |       | Note 7         |
| support  |       | sta    |    |        |       |                |
| bolts    |       | inless |    |        |       |                |
|          |       | steel  |    |        |       |                |
+----------+-------+--------+----+--------+-------+----------------+
| F        |       |        |    |        |       |                |
| asteners |       |        |    |        |       |                |
| Anti     |       |        |    |        |       |                |
| Coi      |       |        |    |        |       |                |
| ncidence |       |        |    |        |       |                |
| Counter  |       |        |    |        |       |                |
| (ACC)    |       |        |    |        |       |                |
+----------+-------+--------+----+--------+-------+----------------+
| Item     | Dr    | Ma     |    | A      | M     | Comments       |
|          | awing | terial | Ma | pplied | argin |                |
|          | n     | and    | te | Load   | of    |                |
|          | umber | temper | ri | (lbf)  | S     |                |
|          |       |        | al |        | afety |                |
|          |       |        | a  |        | (ult) |                |
|          |       |        | ll |        | F     |                |
|          |       |        | ow |        | S=2.0 |                |
|          |       |        | ab |        |       |                |
|          |       |        | le |        |       |                |
|          |       |        | st |        |       |                |
|          |       |        | re |        |       |                |
|          |       |        | ss |        |       |                |
|          |       |        | (  |        |       |                |
|          |       |        | ks |        |       |                |
|          |       |        | i) |        |       |                |
+----------+-------+--------+----+--------+-------+----------------+
| ACC      |       | A-286, | 2  | T      | 0.012 | Total tension  |
| clamps   |       | 0.     | 00 | ension |       | yield, Note 13 |
| to VC    |       | 190-32 |    | = 545  |       |                |
| flange   |       |        |    |        |       |                |
| bolts    |       |        |    | Shear  |       |                |
|          |       |        |    | = 0    |       |                |
+----------+-------+--------+----+--------+-------+----------------+
| PMT      |       | A-286, | 1  | T      | 0.023 | Total tension  |
| supports |       | 0.     | 60 | ension |       | yield, Note 14 |
| to       |       | 190-32 |    | = 246  |       |                |
| Vacuum   |       |        |    |        |       |                |
| Case     |       |        |    | Shear  |       |                |
|          |       |        |    | = 273  |       |                |
+----------+-------+--------+----+--------+-------+----------------+
| F        |       |        |    |        |       |                |
| asteners |       |        |    |        |       |                |
| Zenith   |       |        |    |        |       |                |
| Radiator |       |        |    |        |       |                |
+----------+-------+--------+----+--------+-------+----------------+
| Item     | Dr    | Ma     |    | A      | M     | Comments       |
|          | awing | terial | Ma | pplied | argin |                |
|          | n     | and    | te | Load   | of    |                |
|          | umber | temper | ri | (lbf)  | S     |                |
|          |       |        | al |        | afety |                |
|          |       |        | a  |        | (ult) |                |
|          |       |        | ll |        | F     |                |
|          |       |        | ow |        | S=2.0 |                |
|          |       |        | ab |        |       |                |
|          |       |        | le |        |       |                |
|          |       |        | st |        |       |                |
|          |       |        | re |        |       |                |
|          |       |        | ss |        |       |                |
|          |       |        | (  |        |       |                |
|          |       |        | ks |        |       |                |
|          |       |        | i) |        |       |                |
+----------+-------+--------+----+--------+-------+----------------+
| Sandwich | Joint | A286,  | 1  | t      | 0     | Combined       |
| panel to | 0203  | 0.     | 60 | ension | .37(y | tension and    |
| 3w-IF    |       | 190-32 |    | = 28   | ield) | shear ,        |
| bracket  |       | NAS    |    |        |       |                |
|          |       | 1351N3 |    | Shear  |       | Note 15, page  |
|          |       |        |    | = 299  |       | 77             |
+----------+-------+--------+----+--------+-------+----------------+
| 3w-IF    | Joint | A286,  | 1  | t      | 0.39  | Combined       |
| bracket  | 0305  | 0      | 60 | ension | (y    | tension and    |
| to TRD   |       | .25-28 |    | = 509  | ield) | shear,         |
|          |       | NAS    |    |        |       |                |
|          |       | 1351N4 |    | Shear  |       | Note 15, page  |
|          |       |        |    | = 581  |       | 79             |
+----------+-------+--------+----+--------+-------+----------------+
| Z        | Joint | A286,  | 1  | t      | 0.41  | Combined       |
| bracket  | 0405  | 0.     | 60 | ension | (y    | tension and    |
| to TRD   |       | 190-32 |    | = 227  | ield) | shear,         |
| upper    |       | NAS    |    |        |       |                |
| plate    |       | 1351N3 |    | Shear  |       | Note 15, Page  |
|          |       |        |    | = 161  |       | 80             |
+----------+-------+--------+----+--------+-------+----------------+
| F        |       |        |    |        |       |                |
| asteners |       |        |    |        |       |                |
| Main and |       |        |    |        |       |                |
| Tracker  |       |        |    |        |       |                |
| Radiator |       |        |    |        |       |                |
+----------+-------+--------+----+--------+-------+----------------+
| Item     | Dr    | Ma     |    | A      | M     | Comments       |
|          | awing | terial | Ma | pplied | argin |                |
|          | n     | and    | te | Load   | of    |                |
|          | umber | temper | ri | (lbf)  | S     |                |
|          |       |        | al |        | afety |                |
|          |       |        | a  |        | (ult) |                |
|          |       |        | ll |        | F     |                |
|          |       |        | ow |        | S=2.0 |                |
|          |       |        | ab |        |       |                |
|          |       |        | le |        |       |                |
|          |       |        | st |        |       |                |
|          |       |        | re |        |       |                |
|          |       |        | ss |        |       |                |
|          |       |        | (  |        |       |                |
|          |       |        | ks |        |       |                |
|          |       |        | i) |        |       |                |
+----------+-------+--------+----+--------+-------+----------------+
| USS to   | Joint | A 286  | 1  | T      | 0.32  | Combined       |
| tracker  | 7     | 0.     | 60 | ension |       | Tension and    |
| radiator |       | 250-28 |    | = 73   |       | shear          |
| I/F      |       | NAS    |    |        |       |                |
| brackets |       | 1351N4 |    | Shear  |       | Page 247, Note |
|          |       |        |    | = 794  |       | 16,            |
+----------+-------+--------+----+--------+-------+----------------+
| Tracker  | Joint | A 286  | 1  | T      | 0.54  | Total tension  |
| radiator | 8     | 0.     | 60 | ension |       | yield , Page   |
| panel to |       | 190-32 |    | = 50   |       | 250,           |
| I/F      |       | NAS    |    |        |       |                |
| brackets |       | 1351N3 |    | Shear  |       | Note 16        |
|          |       |        |    | = 147  |       |                |
+----------+-------+--------+----+--------+-------+----------------+
| Tracker  | Joint | MS     | 80 | T      | 0.15  | Combined       |
| radiator | 9     | 51957, |    | ension |       | Tension and    |
| panel to |       |        |    | = 12   |       | shear yield ,  |
| c        |       | 0.     |    |        |       | Page 253, Note |
| ondenser |       | 138-32 |    | Shear  |       | 16             |
| plate    |       |        |    | = 112  |       |                |
+----------+-------+--------+----+--------+-------+----------------+
| Tracker  | Joint | A 286  | 1  | T      | 0.35  | Combined       |
| radiator | 10    | 0.3    | 60 | ension | yield | axial, bending |
| rods to  |       | 125-24 |    | = 265  |       | and shear Page |
| brackets |       | N      |    |        |       | 257, Note 16   |
|          |       | AS6705 |    | Shear  |       |                |
|          |       |        |    | = 254  |       |                |
+----------+-------+--------+----+--------+-------+----------------+
| Main to  | Joint | A286   | 1  | T      | 0.53  | Total tension  |
| tracker  | 11b   | 0.     | 60 | ension |       | yield, Page    |
| radiator |       | 190-32 |    | = 58   |       | 263,           |
| bracket  |       |        |    |        |       |                |
|          |       | NAS    |    | Shear  |       | Note 16        |
|          |       | 1351N3 |    | = 44   |       |                |
+----------+-------+--------+----+--------+-------+----------------+
|          |       |        |    |        |       |                |
+----------+-------+--------+----+--------+-------+----------------+
|          |       |        |    |        |       |                |
+----------+-------+--------+----+--------+-------+----------------+
|          |       |        |    |        |       |                |
+----------+-------+--------+----+--------+-------+----------------+
|          |       |        |    |        |       |                |
+----------+-------+--------+----+--------+-------+----------------+
| F        |       |        |    |        |       |                |
| asteners |       |        |    |        |       |                |
| AMS-02   |       |        |    |        |       |                |
| El       |       |        |    |        |       |                |
| ectronic |       |        |    |        |       |                |
| Crates   |       |        |    |        |       |                |
| and      |       |        |    |        |       |                |
| Radiator |       |        |    |        |       |                |
| Brackets |       |        |    |        |       |                |
+----------+-------+--------+----+--------+-------+----------------+
| Item     | Dr    | Ma     |    | A      | M     | Comments       |
|          | awing | terial | Ma | pplied | argin |                |
|          | n     | and    | te | Load   | of    |                |
|          | umber | temper | ri | (lbf)  | S     |                |
|          |       |        | al |        | afety |                |
|          |       |        | a  |        | (ult) |                |
|          |       |        | ll |        | F     |                |
|          |       |        | ow |        | S=2.0 |                |
|          |       |        | ab |        |       |                |
|          |       |        | le |        |       |                |
|          |       |        | st |        |       |                |
|          |       |        | re |        |       |                |
|          |       |        | ss |        |       |                |
|          |       |        | (  |        |       |                |
|          |       |        | ks |        |       |                |
|          |       |        | i) |        |       |                |
+----------+-------+--------+----+--------+-------+----------------+
| USS to   | Joint | A 286  | 1  | T      | 0.011 | Combined       |
| top      | 1a    | 0      | 60 | ension |       | tension and    |
| Bracket  |       | .25-28 |    | =      |       | shear,         |
|          |       | NAS    |    | 274.7  |       |                |
|          |       | 1351N4 |    |        |       | Page 205, Note |
|          |       |        |    | Shear  |       | 16             |
|          |       |        |    | =      |       |                |
|          |       |        |    | 1145.5 |       |                |
+----------+-------+--------+----+--------+-------+----------------+
| Brackets | Joint | A 286  | 2  | T      | 0.18  | Combined       |
| to       | 2a    | 0.     | 00 | ension |       | tension and    |
| El       |       | 190-32 |    | = 308  |       | shear,         |
| ectronic |       | EWB    |    |        |       |                |
| boxes    |       | 0420-3 |    | Shear  |       | Page 213, Note |
| upper    |       |        |    | = 495  |       | 16             |
+----------+-------+--------+----+--------+-------+----------------+
| Main     | Joint | A 286  | 1  | T      | 0.28  | Combined       |
| Rad      | 3 b   | 0      | 60 | ension |       | tension and    |
| iator/El |       | .25-28 |    | = 60   |       | shear,         |
| ectronic |       | NAS    |    |        |       |                |
| boxes    |       | 1351N4 |    | Shear  |       | Page 222, Note |
| Joints   |       |        |    | =      |       | 16             |
|          |       |        |    | 829.4  |       |                |
+----------+-------+--------+----+--------+-------+----------------+
| Links to | Joint | A 286  | 1  | T      | 0.11  | Combined       |
| el       | 4     | 0.     | 60 | ension |       | shear, tension |
| ectronic |       | 190-32 |    | = 60   |       | and bending,   |
| boxes    |       | NAS    |    |        |       | Page 229, Note |
|          |       | 1351N3 |    | Shear  |       | 16             |
|          |       |        |    | = 557  |       |                |
+----------+-------+--------+----+--------+-------+----------------+
| Crates   | Joint | A 286  | 1  | T      | 0.10  | Total tension  |
| and XPD  | 5a    | 0.     | 60 | ension |       | yield, page    |
| wall     |       | 164-32 |    | = 166  |       | 233,           |
| joints   |       | NAS1   |    |        |       |                |
|          |       | 352N08 |    | Shear  |       | Note 16        |
|          |       |        |    | =58    |       |                |
+----------+-------+--------+----+--------+-------+----------------+
| TPD wall | Joint | A 286  | 1  | T      | 0.12  | Total tension  |
| Joints   | 5b    | 0.     | 60 | ension |       | yield, Page    |
|          |       | 164-32 |    | = 102  |       | 235,           |
|          |       | NAS1   |    |        |       |                |
|          |       | 351N08 |    | Shear  |       | Note 16        |
|          |       |        |    | = 28   |       |                |
+----------+-------+--------+----+--------+-------+----------------+
| Upper T  | Joint | A 286  | 1  | T      | 0.01  | Total tension  |
| crate    | 5c    | 0.     | 60 | ension |       | yield, Page    |
| wall     |       | 190-32 |    | = 855  |       | 237,           |
| Joints   |       | NAS    |    |        |       |                |
|          |       | 1351N3 |    | Shear  |       | Note 16        |
|          |       |        |    | = 376  |       |                |
+----------+-------+--------+----+--------+-------+----------------+
| Lower    | Joint | A-286  | 1  | T      | 0.13  | Combined       |
| Bracket  | 6     | 0.4    | 60 | ension | yield | axial, bending |
| bolt     |       | 375-20 |    | = 702  |       | and shear      |
|          |       |        |    |        |       |                |
|          |       | N      |    | Shear  |       | Page 242, Note |
|          |       | AS6707 |    | = 1    |       | 16             |
+----------+-------+--------+----+--------+-------+----------------+
| F        |       |        |    |        |       |                |
| asteners |       |        |    |        |       |                |
| ECAL and |       |        |    |        |       |                |
| RICH HV  |       |        |    |        |       |                |
| Bricks   |       |        |    |        |       |                |
+----------+-------+--------+----+--------+-------+----------------+
| Item     | Dr    | Ma     | Ma | A      | M     | Comments       |
|          | awing | terial | te | pplied | argin |                |
|          | N     | and    | ri | Load   | of    |                |
|          | umber | temper | al | (lbf)  | S     |                |
|          |       |        | a  |        | afety |                |
|          |       |        | ll |        | (ult) |                |
|          |       |        | ow |        | FS    |                |
|          |       |        | ab |        | =2.0  |                |
|          |       |        | le |        |       |                |
|          |       |        | st |        |       |                |
|          |       |        | re |        |       |                |
|          |       |        | ss |        |       |                |
|          |       |        | (  |        |       |                |
|          |       |        | ks |        |       |                |
|          |       |        | i) |        |       |                |
+----------+-------+--------+----+--------+-------+----------------+
| HV       | Joint | A 286  | 1  | T      | 0.18  | Total tension  |
| Bricks   | 1     | 0      | 60 | ension |       | yield , Note 4 |
| to USS   |       | .25-28 |    | = 245  |       |                |
|          |       | NAS    |    |        |       |                |
|          |       | 1351N4 |    | Shear  |       |                |
|          |       |        |    | = 202  |       |                |
+----------+-------+--------+----+--------+-------+----------------+
| Lateral  | Joint | A4 70  | 1  | T      | 0.11  | Total tension  |
| wall to  | 2     | 0.0984 | 02 | ension |       | yield , Note   |
| bracket  |       | in     |    | = 8    |       | 19             |
|          |       | (2.5   |    |        |       |                |
|          |       | mm)    |    | Shear  |       |                |
|          |       |        |    | = 56   |       |                |
+----------+-------+--------+----+--------+-------+----------------+
| Frame    | Joint | A 4 70 | 1  | T      | 0.02  | Tension yield  |
| and      | 3     | 0.1181 | 02 | ension |       | , Note 19      |
| bracket  |       | in (3  |    | = 130  |       |                |
|          |       | mm)    |    |        |       |                |
|          |       |        |    | Shear  |       |                |
|          |       |        |    | = 114  |       |                |
+----------+-------+--------+----+--------+-------+----------------+
| F        |       |        |    |        |       |                |
| asteners |       |        |    |        |       |                |
| TOF HV   |       |        |    |        |       |                |
| bricks   |       |        |    |        |       |                |
+----------+-------+--------+----+--------+-------+----------------+
| Item     | Dr    | Ma     | Ma | A      | M     | Comments       |
|          | awing | terial | te | pplied | argin |                |
|          | N     | and    | ri | Load   | of    |                |
|          | umber | temper | al | (lbf)  | S     |                |
|          |       |        | a  |        | afety |                |
|          |       |        | ll |        | (ult) |                |
|          |       |        | ow |        | FS    |                |
|          |       |        | ab |        | =2.0  |                |
|          |       |        | le |        |       |                |
|          |       |        | st |        |       |                |
|          |       |        | re |        |       |                |
|          |       |        | ss |        |       |                |
|          |       |        | (  |        |       |                |
|          |       |        | ks |        |       |                |
|          |       |        | i) |        |       |                |
+----------+-------+--------+----+--------+-------+----------------+
| TOF HV   | Joint | A 286  | 1  | T      | 0.16  | Total tension  |
| bricks   | 1     | 0      | 60 | ension |       | yield, Note 4  |
| to       |       | .25-28 |    | = 152  |       |                |
| R        |       | NAS    |    |        |       |                |
| adiators |       | 1351N4 |    | Shear  |       |                |
|          |       |        |    | = 131  |       |                |
+----------+-------+--------+----+--------+-------+----------------+
| Lateral  | Joint | A4 70  | 1  | T      | 0.10  | Total tension  |
| wall to  | 2     | 0.0984 | 02 | ension |       | yield, Note 19 |
| Frame    |       | in     |    | = 26   |       |                |
|          |       | (2.5   |    |        |       |                |
|          |       | mm)    |    | Shear  |       |                |
|          |       |        |    | = 39   |       |                |
+----------+-------+--------+----+--------+-------+----------------+
| Vertical | Joint | A4 70  | 1  | T      | 0.07  | Total tension  |
| stand    | 3     | 0.1181 | 02 | ension |       | yield, Note 19 |
| off to   |       | (3 mm) |    | = 109  |       |                |
| cover    |       |        |    |        |       |                |
|          |       |        |    | Shear  |       |                |
|          |       |        |    | = 84   |       |                |
+----------+-------+--------+----+--------+-------+----------------+
| F        |       |        |    |        |       |                |
| asteners |       |        |    |        |       |                |
| AMS-02   |       |        |    |        |       |                |
| Vacuum   |       |        |    |        |       |                |
| Case     |       |        |    |        |       |                |
| co       |       |        |    |        |       |                |
| mponents |       |        |    |        |       |                |
+----------+-------+--------+----+--------+-------+----------------+
| Item     | Dr    | Ma     | Ma | A      | M     | Comments       |
|          | awing | terial | te | pplied | argin |                |
|          | n     | and    | ri | Load   | of    |                |
|          | umber | temper | al | (lbf)  | S     |                |
|          |       |        | a  |        | afety |                |
|          |       |        | ll |        | (ult) |                |
|          |       |        | ow |        | F     |                |
|          |       |        | ab |        | S=1.4 |                |
|          |       |        | le |        |       |                |
|          |       |        | st |        |       |                |
|          |       |        | re |        |       |                |
|          |       |        | ss |        |       |                |
|          |       |        | (  |        |       |                |
|          |       |        | ks |        |       |                |
|          |       |        | i) |        |       |                |
+----------+-------+--------+----+--------+-------+----------------+
| Upper    | S     | EWB    | 2  | T      | 0.079 | Total tension  |
| Support  | EG391 | 0420   | 00 | ension |       | yield, Sect.   |
| ring to  | 35776 | 0      |    | = 493  |       | 3.10.1-6 Note  |
| conical  |       | .25-28 |    |        |       | 9              |
| flange   |       |        |    | Shear  |       |                |
|          |       |        |    | =540   |       |                |
+----------+-------+--------+----+--------+-------+----------------+
| Lower    | S     | EWB    | 2  | T      | 0.077 | Total tension  |
| Support  | EG391 | 0420   | 00 | ension |       | yield, Sect.   |
| ring to  | 35776 | 0      |    | = 560  |       | 3.10.2-6 Note  |
| conical  |       | .25-28 |    |        |       | 9              |
| flange   |       |        |    | Shear  |       |                |
|          |       |        |    | =815   |       |                |
+----------+-------+--------+----+--------+-------+----------------+
| Upper    | S     | EWB    | 2  | T      | 0.078 | Total tension  |
| Support  | EG391 | 0420   | 00 | ension |       | yield, Sect.   |
| ring to  | 35776 | 0      |    | = 770  |       | 3.10.3-7 Note  |
| outer    |       | .25-28 |    |        |       | 9              |
| cylinder |       |        |    | Shear  |       |                |
|          |       |        |    | =442   |       |                |
+----------+-------+--------+----+--------+-------+----------------+
| Lower    | S     | EWB    | 2  | T      | 0.071 | Total tension  |
| Support  | EG391 | 0420   | 00 | ension |       | yield, Sect.   |
| ring to  | 35776 | 0      |    | = 638  |       | 3.10.4.1-7     |
| outer    |       | .25-28 |    |        |       | Note 9         |
| cylinder |       |        |    | Shear  |       |                |
|          |       |        |    | = 326  |       |                |
+----------+-------+--------+----+--------+-------+----------------+
| Upper    | S     | NA     | 1  | T      | 0.082 | Total tension  |
| I/F      | EG391 | S1956C | 80 | ension |       | yield, Sect.   |
| plate to | 35776 |        |    | = 3343 |       | 3.10.6-11 Note |
| Vacuum   |       | A 286  |    |        |       | 9              |
| case     |       | 0.     |    | Shear  |       |                |
|          |       | 375-24 |    | = 914  |       |                |
+----------+-------+--------+----+--------+-------+----------------+
| Lower    | S     | NA     | 1  | T      | 0.106 | Total tension  |
| I/F      | EG391 | S1956C | 80 | ension |       | yield, Sect.   |
| plate to | 35776 |        |    | = 1376 |       | 3.10.7.1-11,   |
| vacuum   |       | A 286, |    |        |       | Note 9         |
| case     |       | 0.     |    | Shear  |       |                |
|          |       | 375-24 |    | = 136  |       |                |
+----------+-------+--------+----+--------+-------+----------------+
| Lower    | S     | NA     | 1  | T      | 0.103 | Total tension  |
| I/F      | EG391 | S1958C | 80 | ension |       | yield, Sect.   |
| plate to | 35776 |        |    | = 2611 |       | 3.10.7.2-11,   |
| vacuum   |       | A 286, |    |        |       | Note 9         |
| case     |       | 0      |    | Shear  |       |                |
|          |       | .50-20 |    | = 358  |       |                |
+----------+-------+--------+----+--------+-------+----------------+
| Clevis   | S     | NA     | 1  | T      | 0.070 | Total tension  |
| plate to | EG391 | S1958C | 80 | ension |       | yield, Sect.   |
| Upper    | 35776 |        |    | = 5986 |       | 3.10.5-8 Note  |
| support  |       | A 286  |    |        |       | 9              |
| ring     |       | 0.5-20 |    | Shear  |       |                |
|          |       |        |    | = 5323 |       |                |
+----------+-------+--------+----+--------+-------+----------------+
| USS-02   |       |        |    |        |       |                |
| F        |       |        |    |        |       |                |
| asteners |       |        |    |        |       |                |
+----------+-------+--------+----+--------+-------+----------------+
| Item     | Dr    | Ma     | Ma | A      | M     | Comments       |
|          | awing | terial | te | pplied | argin |                |
|          | n     | and    | ri | Load   | of    |                |
|          | umber | temper | al | (lbf)  | S     |                |
|          |       |        | a  |        | afety |                |
|          |       |        | ll |        | (ult) |                |
|          |       |        | ow |        | F     |                |
|          |       |        | ab |        | S=1.4 |                |
|          |       |        | le |        |       |                |
|          |       |        | st |        |       |                |
|          |       |        | re |        |       |                |
|          |       |        | ss |        |       |                |
|          |       |        | (  |        |       |                |
|          |       |        | ks |        |       |                |
|          |       |        | i) |        |       |                |
+----------+-------+--------+----+--------+-------+----------------+
| Upper    | S     | NA     | 1  | T      | 0.033 | Total tension  |
| I/F      | DG391 | S1958C | 80 | ension |       | yield, Sect.   |
| plate to | 35724 |        |    | = 3686 |       | 2.4.1.1-11     |
| USS-02   |       | A 286  |    |        |       | Note 10        |
|          |       | 0      |    | Shear  |       |                |
|          |       | .50-20 |    | = 1112 |       |                |
+----------+-------+--------+----+--------+-------+----------------+
| Lower    | S     | NA     | 1  | T      | 0.046 | Total tension  |
| I/F      | DG391 | S1958C | 80 | ension |       | yield, Sect.   |
| plate to | 35726 |        |    | = 2856 |       | 2.4.1.2-11     |
| USS-02   |       | A 286  |    |        |       | Note 10        |
|          |       | 0      |    | Shear  |       |                |
|          |       | .50-20 |    | = 2294 |       |                |
+----------+-------+--------+----+--------+-------+----------------+
| Sill     | S     | NA     | 1  | T      | 0.065 | Total tension  |
| bracket  | DG391 | S1958C | 80 | ension |       | yield, Sect    |
| to Sill  | 35726 |        |    | = 4907 |       | 2.4.1.4-11     |
| joint    |       | A 286  |    |        |       | Note 10        |
|          |       | 0      |    | Shear  |       |                |
|          |       | .50-20 |    | = 65   |       |                |
+----------+-------+--------+----+--------+-------+----------------+
| Lower    | S     | NA     | 1  | T      | 0.033 | Joint          |
| USS to   | DG391 | S1958C | 80 | ension |       | Separation,    |
| Upper    | 35724 |        |    | = 6136 |       | Sect.          |
| USS      |       | A 286  |    |        |       | 2.4.2.1-11,    |
| bolts    |       | 0      |    | Shear  |       | Note 10        |
|          |       | .50-20 |    | = 2952 |       |                |
+----------+-------+--------+----+--------+-------+----------------+
| Lower    | S     | E      | 2  | T      | 0.055 | Total tension  |
| angle    | DG391 | WB0420 | 00 | ension |       | yield,         |
| beam to  | 35758 |        |    | = 7677 |       | S              |
| ce       |       | 0      |    |        |       | ect.2.4.2.2-11 |
| nterbody |       | .50-20 |    | Shear  |       | Note 10        |
| box      |       |        |    | = 436  |       |                |
| joint    |       |        |    |        |       |                |
+----------+-------+--------+----+--------+-------+----------------+
| Diagonal | S     | E      | 2  | T      | 0.015 | Total tension  |
| sill     | DG391 | WB0420 | 00 | ension |       | yield,         |
| bracket  | 35726 |        |    | =      |       | S              |
| to sill  |       | 0      |    | 12428  |       | ect.2.4.1.5-11 |
| joint    |       | .50-20 |    |        |       | Note 10.       |
|          |       |        |    | Shear  |       | Negative M.S.  |
|          |       |        |    | = 2029 |       | on Joint       |
|          |       |        |    |        |       | separation.    |
|          |       |        |    |        |       | Ref. sect      |
|          |       |        |    |        |       | 2.4.1.5-12 for |
|          |       |        |    |        |       | acceptance     |
|          |       |        |    |        |       | rationale      |
+----------+-------+--------+----+--------+-------+----------------+
| Keel and |       |        |    |        |       |                |
| PAS      |       |        |    |        |       |                |
| F        |       |        |    |        |       |                |
| asteners |       |        |    |        |       |                |
+----------+-------+--------+----+--------+-------+----------------+
| Item     | Dr    | Ma     | Ma | A      | M     | Comments       |
|          | awing | terial | te | pplied | argin |                |
|          | n     | and    | ri | Load   | of    |                |
|          | umber | temper | al | (lbf)  | S     |                |
|          |       |        | a  |        | afety |                |
|          |       |        | ll |        | (ult) |                |
|          |       |        | ow |        | F     |                |
|          |       |        | ab |        | S=1.4 |                |
|          |       |        | le |        |       |                |
|          |       |        | st |        |       |                |
|          |       |        | re |        |       |                |
|          |       |        | ss |        |       |                |
|          |       |        | (  |        |       |                |
|          |       |        | ks |        |       |                |
|          |       |        | i) |        |       |                |
+----------+-------+--------+----+--------+-------+----------------+
| Keel     | S     | E      | 2  | T      | 0.068 | Total thread   |
| angle    | EG391 | WB0420 | 00 | ension |       | shear, Sect.   |
| joint to | 35724 | 0      |    | = 1883 |       | 2.4.3.1-11,    |
| lower    |       | .50-20 |    |        |       | Note 9         |
| USS      |       |        |    | Shear  |       |                |
| assembly |       |        |    | = 1752 |       |                |
+----------+-------+--------+----+--------+-------+----------------+
| Keel     | S     | NAS8   | 1  | T      | 0.076 | Total tension  |
| retainer | EG391 | 103PU8 | 60 | ension |       | yield, Sect.   |
| to keel  | 35768 |        |    | = 328  |       | 2.4.3.2-7,     |
|          |       | 0.     |    |        |       | Note 9         |
| Trunnion |       | 190-32 |    | Shear  |       |                |
| and keel |       |        |    | = 0    |       |                |
| block    |       |        |    |        |       |                |
+----------+-------+--------+----+--------+-------+----------------+
| PAS      | S     | NAS13  | 1  | T      | 0.091 | Total tension  |
| Handle   | EG391 | 51N4-8 | 60 | ension |       | yield, sect    |
| to       | 35849 |        |    | = 803  |       | 4.12.2 Note 11 |
| handle   |       | 0      |    |        |       |                |
|          |       | .25-28 |    | Shear  |       |                |
| E        |       |        |    | = 0.0  |       |                |
| xtension |       |        |    |        |       |                |
| bolts    |       |        |    |        |       |                |
+----------+-------+--------+----+--------+-------+----------------+
| PAS      | S     | NAS    | 1  | T      | 0.175 | Total tension  |
| guide    | EG391 | 1351N6 | 60 | ension |       | yield,         |
| pins to  | 35815 |        |    | = 523  |       | sect.4.12.5.1  |
| platform |       | 0.     |    |        |       | Note 11        |
|          |       | 375-24 |    | Shear  |       |                |
|          |       |        |    | = 473  |       |                |
+----------+-------+--------+----+--------+-------+----------------+
| F        |       |        |    |        |       |                |
| asteners |       |        |    |        |       |                |
| AMS-02   |       |        |    |        |       |                |
| UPS      |       |        |    |        |       |                |
+----------+-------+--------+----+--------+-------+----------------+
| Item     | Dr    | Ma     | Ma | Max.   | M     | Comments       |
|          | awing | terial | te | a      | argin |                |
|          | n     | and    | ri | pplied | of    |                |
|          | umber | temper | al | Load   | S     |                |
|          |       |        | a  | (lbf)  | afety |                |
|          |       |        | ll |        | (ult) |                |
|          |       |        | ow |        | F     |                |
|          |       |        | ab |        | S=2.0 |                |
|          |       |        | le |        |       |                |
|          |       |        | st |        |       |                |
|          |       |        | re |        |       |                |
|          |       |        | ss |        |       |                |
|          |       |        | (  |        |       |                |
|          |       |        | ks |        |       |                |
|          |       |        | i) |        |       |                |
+----------+-------+--------+----+--------+-------+----------------+
| UPS box  |       | A-286  | 1  | T      | 0.22  | Total tension  |
| to       |       | 0      | 60 | ension |       | yield, Note    |
| bracket  |       | .25-28 |    | = 117  |       | 18, page 10    |
| bolts    |       | NAS    |    |        |       |                |
|          |       | 1351N4 |    | Shear  |       |                |
|          |       |        |    | = 250  |       |                |
+----------+-------+--------+----+--------+-------+----------------+
| Bracket  |       | A-286  | 1  | T      | 0.34  | Total tension  |
| to USS   |       | 0      | 80 | ension |       | yield, Note    |
| bolts    |       | .25-28 |    | = 141  |       | 18, page 10    |
|          |       |        |    |        |       |                |
|          |       | NA     |    | Shear  |       |                |
|          |       | S1954C |    | = 128  |       |                |
+----------+-------+--------+----+--------+-------+----------------+
| F        |       |        |    |        |       |                |
| asteners |       |        |    |        |       |                |
| AMS-02   |       |        |    |        |       |                |
| E-Crate  |       |        |    |        |       |                |
+----------+-------+--------+----+--------+-------+----------------+
| Item     | Dr    | Ma     | Ma | A      | M     | Comments       |
|          | awing | terial | te | pplied | argin |                |
|          | n     | and    | ri | Load   | of    |                |
|          | umber | temper | al | (lbf)  | S     |                |
|          |       |        | a  |        | afety |                |
|          |       |        | ll |        | (ult) |                |
|          |       |        | ow |        | F     |                |
|          |       |        | ab |        | S=2.0 |                |
|          |       |        | le |        |       |                |
|          |       |        | st |        |       |                |
|          |       |        | re |        |       |                |
|          |       |        | ss |        |       |                |
|          |       |        | (  |        |       |                |
|          |       |        | ks |        |       |                |
|          |       |        | i) |        |       |                |
+----------+-------+--------+----+--------+-------+----------------+
| E-Crates | Joint | A 286  | 1  | T      | 0.09  | Joint          |
| to       | 1     | 0.     | 60 | ension |       | separation,    |
| USS-02   |       | 190-32 |    | = 601  |       | Note 4         |
|          |       | NAS    |    |        |       |                |
|          |       | 1351N3 |    | Shear  |       |                |
|          |       |        |    | = 124  |       |                |
+----------+-------+--------+----+--------+-------+----------------+
| Lateral  | Joint | A 286  | 1  | T      | 0.13  | Total tension  |
| walls to | 2     | 0.     | 60 | ension |       | yield, Note 4  |
| bottom   |       | 190-32 |    | = 272  |       |                |
| plate    |       | NAS    |    |        |       |                |
|          |       | 1351N3 |    | Shear  |       |                |
|          |       |        |    | = 339  |       |                |
+----------+-------+--------+----+--------+-------+----------------+
| Lateral  | Joint | A286   | 1  | T      | 0.12  | Total tension  |
| walls    | 3     | 0.     | 60 | ension |       | yield, Note 4  |
|          |       | 164-32 |    | = 196  |       |                |
|          |       |        |    |        |       |                |
|          |       | NAS1   |    | Shear  |       |                |
|          |       | 352N08 |    | = 157  |       |                |
+----------+-------+--------+----+--------+-------+----------------+
| F        |       |        |    |        |       |                |
| asteners |       |        |    |        |       |                |
| Cr       |       |        |    |        |       |                |
| yomagnet |       |        |    |        |       |                |
| Avionics |       |        |    |        |       |                |
| Box      |       |        |    |        |       |                |
| (CAB)    |       |        |    |        |       |                |
+----------+-------+--------+----+--------+-------+----------------+
| Item     | Dr    | Ma     | Ma | A      | M     | Comments       |
|          | awing | terial | te | pplied | argin |                |
|          | n     | and    | ri | Load   | of    |                |
|          | umber | temper | al | (lbf)  | S     |                |
|          |       |        | a  |        | afety |                |
|          |       |        | ll |        | (ult) |                |
|          |       |        | ow |        | F     |                |
|          |       |        | ab |        | S=2.0 |                |
|          |       |        | le |        |       |                |
|          |       |        | st |        |       |                |
|          |       |        | re |        |       |                |
|          |       |        | ss |        |       |                |
|          |       |        | (  |        |       |                |
|          |       |        | ks |        |       |                |
|          |       |        | i) |        |       |                |
+----------+-------+--------+----+--------+-------+----------------+
| CAB to   |       | A 286  | 1  | T      | 0.30  | yield, Note    |
| USS-02   |       | 0.2    | 80 | ension |       | 12, Page 40    |
|          |       | 50-28, |    | = 305  |       |                |
|          |       | NAS    |    |        |       |                |
|          |       | 1954C4 |    | Shear  |       |                |
|          |       |        |    | = 338  |       |                |
+----------+-------+--------+----+--------+-------+----------------+
| Assembly |       | AISI   | 1  | T      | 0.03  | yield, Note    |
| screws   |       | 304    | 01 | ension |       | 12, page 40    |
| Rear     |       | M3x7.5 | .5 | = 121  |       |                |
| frame    |       |        |    |        |       |                |
| modules  |       |        |    | Shear  |       |                |
|          |       |        |    | = 83   |       |                |
+----------+-------+--------+----+--------+-------+----------------+
| PCB      |       | AISI   | 1  | T      | 0.18  | Yield Note 12, |
| s        |       | 304    | 01 | ension |       | Page 40        |
| tiffener |       | M2.5x8 | .5 | = 5    |       |                |
| screws   |       |        |    |        |       |                |
|          |       |        |    | Shear  |       |                |
|          |       |        |    | = 54   |       |                |
+----------+-------+--------+----+--------+-------+----------------+

NOTE:

1\) Ref. TRD fastener analysis summary Excel tables, 6/8/2005

2\) Ref. Box S May_2004_Rev1_doc, Appendix 2

3\) Ref. C_Box \_FEM Analysis, Appendix 1, June 10, 2004

4\) Ref. AMS-02 Bolt Analysis\_ Update_v4(1), Excel tables, 8/14/2005

5\) Ref. ASTS_July 2004_Rev1.doc, Appendix 2, INFN Rome

6\) Ref. Baffle report April 2005_rev 1.doc, appendix 1, INFN Rome

7\) Reference summary of Structural Analysis of AMS-02 Super conducting
Magnet, September 2003, issue 02

8\) Ref. Report ESCG-4450-05-STAN-DOC-0131, Table 3-15, January 2006

9\) Ref. Strength and Stability of Vacuum Case Assembly report

10\) Ref. Strength and Stability for USS-02 analysis report

11\) Ref. PAS analysis report

12\) Ref. Cryomagnet Avionics Box Mechanical Analysis, CAB-AN-CRS-0055,
issue 2, 22 Sept.2006

13\) Ref. ACC-Clamps, Mathcad analysis, 7/15/2005

14\) Ref. PMT-Supp, Mathcad analysis, 7/15/2005

15\) Ref. Zenith Radiator Structural analysis report, AMS-OHB-SAR-001,
issue 4, 1 April 2005

16\) Ref. Main Radiator Structural analysis Report, AMS-02-RP-CGS-005,
issue 4, April 5, 2007

17\) Ref. AMS-02 Tracker Bolt analysis Memo, University of Geneva,
1/26/2006

18\) Ref. UPS Box Redesign Structure Analysis Report, 28 December, 2005,
CSIST Taiwan

19\) Ref. AMS-02-DC-CGS-001, issue 1, Page 3

**Fracture Classification for TRD Structure**

<table>
<colgroup>
<col style="width: 11%" />
<col style="width: 9%" />
<col style="width: 10%" />
<col style="width: 7%" />
<col style="width: 9%" />
<col style="width: 10%" />
<col style="width: 8%" />
<col style="width: 9%" />
<col style="width: 7%" />
<col style="width: 14%" />
</colgroup>
<thead>
<tr class="header">
<th>Item</th>
<th>Drawing number</th>
<th>Material and temper</th>
<th>Material allowable stress (ksi)</th>
<th>Max. applied stress (ksi)</th>
<th>Ratio of applied limit stress to allowable stress</th>
<th>Margin of Safety (ult) FS=2.0</th>
<th>Fracture Classification</th>
<th>Rationale</th>
<th>Comments</th>
</tr>
</thead>
<tbody>
<tr class="odd">
<td colspan="10"><strong>TRD Support</strong></td>
</tr>
<tr class="even">
<td>M structure</td>
<td>1811/60_0002_1_V1</td>
<td>7075-T7351</td>
<td>62</td>
<td>15.4</td>
<td>0.25</td>
<td>1.02</td>
<td>Low risk</td>
<td>Note 2</td>
<td>Page 31, Note 4</td>
</tr>
<tr class="odd">
<td>Corner brackets</td>
<td>1811/60_0001_1_V1</td>
<td>7075-T7351</td>
<td>57</td>
<td>22.9</td>
<td>0.40</td>
<td>0.24</td>
<td>Low risk</td>
<td>Note 2</td>
<td>Page 12, Note 12</td>
</tr>
<tr class="even">
<td>Upper bracket right</td>
<td>1811/60_0003_01_V1</td>
<td>7075-T7351</td>
<td>60</td>
<td>22.8</td>
<td>0.38</td>
<td>0.32</td>
<td>Low risk</td>
<td>Note 2</td>
<td>Page 14, Note 12</td>
</tr>
<tr class="odd">
<td>Upper bracket left</td>
<td>1811/60_0004_01_V1</td>
<td>7075-T7351</td>
<td>60</td>
<td>22.8</td>
<td>0.38</td>
<td>0.32</td>
<td>Low risk</td>
<td>Note 2</td>
<td>Page 14, Note 12</td>
</tr>
<tr class="even">
<td colspan="10"><strong>TRD Octagon</strong></td>
</tr>
<tr class="odd">
<td>Octagon panels</td>
<td>ams1912i-3d-02 ams1912p</td>
<td>Carbon fiber skin Al. 5056 core 1/8 in. cell</td>
<td>145</td>
<td>72.3</td>
<td>0.50</td>
<td>0.002</td>
<td>Low risk</td>
<td>Note 6</td>
<td>Page 20, Note 12</td>
</tr>
<tr class="even">
<td>Octagon panel flanges</td>
<td>ams 02 1912p Detail U,V</td>
<td>Carbon fiber skin Al. 5056 core 1/8 in. cell</td>
<td>145</td>
<td>43.7</td>
<td>0.30</td>
<td>0.66</td>
<td>Low risk</td>
<td>Note 6</td>
<td>Page 24, Note 4</td>
</tr>
<tr class="odd">
<td>Upper flange reinforcement ring</td>
<td>ams 02 1996f</td>
<td>T300 EP fabric</td>
<td>116</td>
<td>-27.7</td>
<td>0.24</td>
<td>1.10</td>
<td>Low risk</td>
<td>Note 6</td>
<td>Page 25, Note 4</td>
</tr>
<tr class="even">
<td>Upper Cover</td>
<td>ams 02 1942g</td>
<td>Carbon fiber skin Al. 5056 core 3/16 cell</td>
<td>116</td>
<td>-32.2</td>
<td>0.28</td>
<td>0.8</td>
<td>Low risk</td>
<td>Note 6</td>
<td>Page 27, Note 4</td>
</tr>
<tr class="odd">
<td colspan="10"><strong>Fasteners</strong></td>
</tr>
<tr class="even">
<td>Item</td>
<td>Drawing number</td>
<td>Material and temper</td>
<td>Material allowable stress (ksi)</td>
<td>Max. applied loads (lbf)</td>
<td>Ratio of applied limit stress to allowable yield stress</td>
<td><p>Margin of</p>
<p>Safety (ult)</p>
<p>F.S.=1.0</p></td>
<td>Fracture classification</td>
<td>Rationale</td>
<td>Comments</td>
</tr>
<tr class="odd">
<td>Upper bracket to M structure</td>
<td></td>
<td>A286, 1/4-28</td>
<td>160</td>
<td>Tension = 1049 Shear = 12</td>
<td>0.84</td>
<td>0.36</td>
<td>Fail-safe</td>
<td>Note 3</td>
<td>Joint Separation, Note 9, Load case 1008</td>
</tr>
<tr class="even">
<td>Corner bracket to M structure</td>
<td></td>
<td>A286, 5/16-24</td>
<td>200</td>
<td>Tension = 2921 Shear = 133</td>
<td>0.79</td>
<td>0.12</td>
<td>Fail-safe</td>
<td>Note 3</td>
<td>Total thread shear, Note 9, Load case 4058</td>
</tr>
<tr class="odd">
<td>Upper brackets to Upper Cover</td>
<td></td>
<td>A286, 1/4-28</td>
<td>140</td>
<td>Tension = 807 Shear = 7</td>
<td>0.88</td>
<td>0.39</td>
<td>Fail-safe</td>
<td>Note 3</td>
<td>Joint Separation, Note 9, Load case 1008</td>
</tr>
<tr class="even">
<td>Upper cover to Octagon</td>
<td></td>
<td>A286, 5/16-24</td>
<td>140</td>
<td>Tension = 158 Shear = 906</td>
<td>0.84</td>
<td>0.55</td>
<td>Fail-safe</td>
<td>Note 3</td>
<td>Combined shear and tension, Note 9, Load case 1008</td>
</tr>
<tr class="odd">
<td>Corner bracket to Upper VC joint</td>
<td>SDG39135720</td>
<td><p>NAS1958C</p>
<p>A286, 1/2-20</p></td>
<td>180</td>
<td>Tension = 3749 Shear = 1254</td>
<td>0.88</td>
<td>0.086</td>
<td>Fail-safe</td>
<td>Note 3</td>
<td>Combined tension and shear, Note10, page 2.4.1.3-21</td>
</tr>
</tbody>
</table>

**Fracture Classification of TRD Gas System structure**

<table>
<colgroup>
<col style="width: 11%" />
<col style="width: 9%" />
<col style="width: 10%" />
<col style="width: 7%" />
<col style="width: 9%" />
<col style="width: 10%" />
<col style="width: 8%" />
<col style="width: 9%" />
<col style="width: 7%" />
<col style="width: 14%" />
</colgroup>
<tbody>
<tr class="odd">
<td>Item</td>
<td>Drawing number</td>
<td>Material and temper</td>
<td>Material allowable stress (ksi)</td>
<td>Max. applied tensile stress (ksi)</td>
<td>Ratio of applied limit stress to allowable stress</td>
<td>Margin of Safety (ult) FS=2.0</td>
<td>Fracture Classification</td>
<td>Rationale</td>
<td>Comments</td>
</tr>
<tr class="even">
<td colspan="10"><strong>TRD Gas System Structures</strong></td>
</tr>
<tr class="odd">
<td>Box S plate</td>
<td></td>
<td>7050-T7451</td>
<td>66.1</td>
<td>30.6</td>
<td>0.46</td>
<td>0.08</td>
<td>Low risk</td>
<td>Note 2</td>
<td>Page 21, Note 5</td>
</tr>
<tr class="even">
<td>Xe tank bracket</td>
<td></td>
<td>6061-T6</td>
<td>42</td>
<td>4.6</td>
<td>0.20</td>
<td>1.40</td>
<td>Low risk</td>
<td>Note 2</td>
<td>Page 21, Note 5</td>
</tr>
<tr class="odd">
<td>Lower bracket</td>
<td></td>
<td>7050-T7451</td>
<td>66.1</td>
<td>12.3</td>
<td>0.18</td>
<td>1.69</td>
<td>Low risk</td>
<td>Note 2</td>
<td>Page 21, Note 5</td>
</tr>
<tr class="even">
<td>Box C base plate</td>
<td></td>
<td>6061-T6</td>
<td>49.3</td>
<td>20.3</td>
<td>0.41</td>
<td>0.21</td>
<td>Low risk</td>
<td>Note 2</td>
<td>Page 15, Note 7</td>
</tr>
<tr class="odd">
<td>Valve bracket</td>
<td></td>
<td>6061-T6</td>
<td>49.3</td>
<td>13.2</td>
<td>0.27</td>
<td>0.86</td>
<td>Low risk</td>
<td>Note 2</td>
<td>Page 15, Note 7</td>
</tr>
<tr class="even">
<td colspan="10"><strong>Fasteners</strong></td>
</tr>
<tr class="odd">
<td>Item</td>
<td>Drawing number</td>
<td>Material and temper</td>
<td>Material allowable stress (ksi)</td>
<td>Applied Load (lbf)</td>
<td>Ratio of applied limit stress to allowable yield stress</td>
<td>Margin of Safety (ult) FS=1.0</td>
<td>Fracture Classification</td>
<td>Rationale</td>
<td>Comments</td>
</tr>
<tr class="even">
<td>Box S/Box C plate to USS upper I/F bolts</td>
<td></td>
<td>NAS1954 0.25-28 A-286</td>
<td>180</td>
<td><p>Tension = 44</p>
<p>Shear = 1680</p></td>
<td>0.89</td>
<td>0.52</td>
<td>Fail-safe</td>
<td>Note 3</td>
<td>Combined tension and shear, Note 8, page 10</td>
</tr>
<tr class="odd">
<td>Box S Xe bracket to plate bolts</td>
<td></td>
<td>NAS1351N6 0.375-24 A-286</td>
<td>160</td>
<td>Tension = 1461 Shear = 445</td>
<td>0.92</td>
<td>0.40</td>
<td>Fail-safe</td>
<td>Note 3</td>
<td>Combined tension and shear, Note 8, page 20</td>
</tr>
<tr class="even">
<td rowspan="2">Box C mounting of cylinder to bracket</td>
<td rowspan="2"></td>
<td rowspan="2"><p>NAS1351N3</p>
<p>0.190-32 A-286</p></td>
<td rowspan="2">160</td>
<td rowspan="2">Tension = 25 Shear = 74</td>
<td rowspan="2">0.87</td>
<td rowspan="2">0.75</td>
<td rowspan="2">Fail-safe</td>
<td>Note 3</td>
<td rowspan="2">Combined tension and shear Note 11, Page 6,</td>
</tr>
<tr class="odd">
<td></td>
</tr>
<tr class="even">
<td>Box C mounting of valve bracket to holder</td>
<td></td>
<td>NAS1351N3 0.190-32 A-286</td>
<td>160</td>
<td>Tension = 73 Shear = 77</td>
<td>0.89</td>
<td>0.36</td>
<td>Fail-safe</td>
<td>Note 3</td>
<td>Combined tension and shear Note 11, Page 15</td>
</tr>
</tbody>
</table>

Notes: (TRD Structure and Gas System)

1\) The components will be classified as per JSC25863A, August 1998 to
comply with NASA-STD-5003, October 1996 and SSP 30558 Rev. B, June 1994.

2\) The component will be classified as low risk as per section 5.1.L.1,
5.1.L.2.A and 5.1.L.2.B.3 of JSC 25863A and will be shown that the
component possesses acceptable durability (Possesses acceptable
resistance to crack growth)

3\) The component will be classified as fail-safe as per section 5.1.c
of JSC 25863A

4\) Ref. Transition Radiation Detector (TRD) Structural Verification
Presentation Rev. 3, 11 April 2005

5\) Ref. TRD Gas system, Box S mechanical Structure AMS-02, Rev_1 27
June 2005, INFN, Rome and MIT

6\) The component will be classified as low risk as per section 5.2 d of
JSC25863A

7\) Ref. Finite Element Analysis for Box-C of TRD Gas System, MIT@CERN,
11 June 2004

8\) Ref. Appendix 2_Box_S May_2004_Rev1_doc,

9\) Ref. TRD fasteners summary Excel tables , 6/8/2005

10\) Ref. Strength and stability analysis report for USS-02

11\) Ref. Appendix1, C_box_FEM analysis, June 10, 2004

12\) Ref. Transition Radiation Detector (TRD) Structural Verification
Presentation , Rev. 5, 7 March 2007

**Fracture Classification of AMS-02 Upper Time of Flight (UTOF)**

<table>
<colgroup>
<col style="width: 11%" />
<col style="width: 9%" />
<col style="width: 10%" />
<col style="width: 7%" />
<col style="width: 9%" />
<col style="width: 10%" />
<col style="width: 8%" />
<col style="width: 9%" />
<col style="width: 7%" />
<col style="width: 14%" />
</colgroup>
<tbody>
<tr class="odd">
<td>Item</td>
<td>Drawing number</td>
<td>Material and temper</td>
<td>Material allowable stress (ksi)</td>
<td>Max. applied tensile stress (ksi)</td>
<td>Ratio of applied limit stress to allowable stress</td>
<td>Margin of Safety (ult) FS=2.0</td>
<td>Fracture Classification</td>
<td>Rationale</td>
<td>Comments</td>
</tr>
<tr class="even">
<td>Upper brackets</td>
<td>ams TOF 08-01-006 UT</td>
<td>7075-T7351</td>
<td>64</td>
<td>31.4</td>
<td>0.49</td>
<td>0.02</td>
<td>Low risk</td>
<td>Note 2</td>
<td>Page 57, Note 4</td>
</tr>
<tr class="odd">
<td>Lower brackets</td>
<td>ams TOF 08-01-001 UT</td>
<td>7075-T7351</td>
<td>64</td>
<td>16.0</td>
<td>0.25</td>
<td>0.98</td>
<td>Low risk</td>
<td>Note 2</td>
<td>Page 57, Note 4</td>
</tr>
<tr class="even">
<td>Extensions</td>
<td>ams TOF 08-01-008 UT</td>
<td>7075-T7351</td>
<td>64</td>
<td>16.1</td>
<td>0.25</td>
<td>0.98</td>
<td>Low risk</td>
<td>Note 2</td>
<td>Page 57, Note 4</td>
</tr>
<tr class="odd">
<td>Honeycomb skins</td>
<td>ams TOF 08-02-002 UT</td>
<td>2024-T81</td>
<td>62.9</td>
<td>18.3</td>
<td>0.29</td>
<td>0.72</td>
<td>Low risk</td>
<td>Note 2</td>
<td>Page 57, Note 4</td>
</tr>
<tr class="even">
<td>Secondary Brackets</td>
<td>ams TOF 02-01-005 UT</td>
<td>7075-T7351</td>
<td>64</td>
<td>8.1</td>
<td>0.12</td>
<td>2.92</td>
<td>Low risk</td>
<td>Note 2</td>
<td>Page 57, Note 4</td>
</tr>
<tr class="odd">
<td>Sensor Boxes</td>
<td>ams TOF 09-001 UT</td>
<td><p>CFRP T300</p>
<p>fabric</p></td>
<td><p>115.9</p>
<p>115.9</p>
<p>14.3</p></td>
<td><p>X=4.9</p>
<p>Y=7.4</p>
<p>XY=4.6</p></td>
<td><p>0.04</p>
<p>0.06</p>
<p>0.32</p></td>
<td>0.51</td>
<td>Low risk</td>
<td>Note 5</td>
<td>Page 58, Note 4, Margin of safety, Note 6</td>
</tr>
<tr class="even">
<td>Scintillator supports</td>
<td></td>
<td>CFRP T 300 fabric</td>
<td><p>115.9</p>
<p>115.9</p>
<p>14.3</p></td>
<td><p>X=22.2</p>
<p>Y=25.7</p>
<p>XY=3.8</p></td>
<td><p>0.01</p>
<p>0.01</p>
<p>0.06</p></td>
<td>0.11</td>
<td>Low risk</td>
<td>Note 5</td>
<td>Page 58, Note 4, Margin of safety, Note 6</td>
</tr>
<tr class="odd">
<td>PMT Box Supports</td>
<td>ams TOF 05-05-001 UT</td>
<td>CFRP T 300 fabric</td>
<td><p>115.9</p>
<p>115.9</p>
<p>14.3</p></td>
<td><p>X=10.4</p>
<p>Y=9.75</p>
<p>XY=2.4</p></td>
<td><p>0.19</p>
<p>0.08</p>
<p>0.17</p></td>
<td>1.7</td>
<td>Low risk</td>
<td>Note 5</td>
<td>Page 58, Note 4, Margin of safety, Note 6</td>
</tr>
<tr class="even">
<td colspan="10"><strong>UTOF Fasteners</strong></td>
</tr>
<tr class="odd">
<td>Item</td>
<td>Drawing number</td>
<td>Material and temper</td>
<td>Material allowable stress (ksi)</td>
<td>Applied Load (lbf)</td>
<td>Ratio of applied limit stress to allowable yield stress</td>
<td>Margin of Safety (ult) FS=1.0</td>
<td>Fracture Classification</td>
<td>Rationale</td>
<td>Comments</td>
</tr>
<tr class="even">
<td>UTOF/TRD I/F bolts</td>
<td>Joint 1</td>
<td>EWB0420-5 0.3125-24</td>
<td>200</td>
<td>Tension = 5292 Shear = 0</td>
<td>0.86</td>
<td>0.11</td>
<td>Fail-safe</td>
<td>Note 3</td>
<td>Total thread shear Note 7</td>
</tr>
<tr class="odd">
<td>Bracket to Ext. bolts</td>
<td>Joint 3</td>
<td><p>NAS1351N4</p>
<p>A-286 0.25-28</p></td>
<td>160</td>
<td><p>Tension = 1091</p>
<p>shear =1922</p></td>
<td>0.83</td>
<td>0.04</td>
<td>Fail-safe</td>
<td>Note 3</td>
<td>Combined tension and shear, Note 7</td>
</tr>
<tr class="even">
<td>Upper to lower bracket bolts</td>
<td>Joint 4</td>
<td><p>NAS1351N4</p>
<p>A-286 0.25-28</p></td>
<td>160</td>
<td>Tension = 674 Shear = 1407</td>
<td>0.80</td>
<td>0.24</td>
<td>Fail-safe</td>
<td>Note 3</td>
<td>Combined tension and shear, Note 7</td>
</tr>
</tbody>
</table>

Notes:

1\) The components will be classified as per JSC 25863 A, August 1998 to
comply with NASA-STD-5003, October 1996 and SSP 30558 Rev. B, June 1994

2\) The component will be classified as low risk as per section 5.1.L.1,
5.1.L.2.A and 5.1.L 2.B.3 of JSC 25863 A and will be shown that the
component possesses acceptable durability (Possesses acceptable
resistance to crack growth)

3\) The component will be classified as fail-safe as per section 5.1 c
of JSC 25863 A

4\) Ref. Upper Time of Flight Structural Analysis Report,
RICSYS-CGS-013, issue 1 , 29 June 2004

5\) The component will be classified as low risk per section 5.2 d of
JSC 25863 A

6\) Tsai_Hill equation shown in note 4 , page 38. Margin of safety is
(1/Failure Index)-1

7\) Ref. AMS-02 Bolt Analysis_Update_v4.(1), 8/4/2005

Fracture Classification of AMS-02 Lower Time of Flight (LTOF)

<table>
<colgroup>
<col style="width: 10%" />
<col style="width: 11%" />
<col style="width: 11%" />
<col style="width: 7%" />
<col style="width: 10%" />
<col style="width: 10%" />
<col style="width: 8%" />
<col style="width: 9%" />
<col style="width: 6%" />
<col style="width: 14%" />
</colgroup>
<thead>
<tr class="header">
<th>Item</th>
<th>Drawing number</th>
<th>Material and temper</th>
<th>Material allowable stress (ksi)</th>
<th>Max. applied tensile stress (ksi)</th>
<th>Ratio of applied limit stress to allowable stress</th>
<th>Margin of Safety (ult) FS=2.0</th>
<th>Fracture Classification</th>
<th>Rationale</th>
<th>Comments</th>
</tr>
</thead>
<tbody>
<tr class="odd">
<td>Beam A</td>
<td>ams TOF 04-01-001 LT</td>
<td>7075-T7351</td>
<td>64</td>
<td>30.6</td>
<td>0.48</td>
<td>0.05</td>
<td>Low risk</td>
<td>Note 2</td>
<td>Page 76, Note 4</td>
</tr>
<tr class="even">
<td>Beam B</td>
<td>ams TOF 04-01-002 LT</td>
<td>7075-T7351</td>
<td>64</td>
<td>29.8</td>
<td>0.46</td>
<td>0.07</td>
<td>Low risk</td>
<td>Note 2</td>
<td>Page 76, Note 4</td>
</tr>
<tr class="odd">
<td>Corner beam</td>
<td>ams TOF 04-01-003 LT</td>
<td>7075-T7351</td>
<td>64</td>
<td>11.0</td>
<td>0.17</td>
<td>1.9</td>
<td>Low risk</td>
<td>Note 2</td>
<td>Page 76, Note 4</td>
</tr>
<tr class="even">
<td>Upper bracket</td>
<td>ams TOF 04-01-021 LT</td>
<td>7075-T7351</td>
<td>64</td>
<td>10.7</td>
<td>0.17</td>
<td>1.98</td>
<td>Low risk</td>
<td>Note 2</td>
<td>Page 76, Note 4</td>
</tr>
<tr class="odd">
<td>Lower bracket</td>
<td>ams TOF 04-01-020 LT</td>
<td>7075-T7351</td>
<td>64</td>
<td>10.0</td>
<td>0.16</td>
<td>&gt;2.0</td>
<td>Low risk</td>
<td>Note 2</td>
<td>Page 76, Note 4</td>
</tr>
<tr class="even">
<td>Internal bracket</td>
<td>ams TOF 04-01-018 LT</td>
<td>7075-T7351</td>
<td>64</td>
<td>13.30</td>
<td>0.21</td>
<td>1.4</td>
<td>Low risk</td>
<td>Note 2</td>
<td>Page 76, Note 4</td>
</tr>
<tr class="odd">
<td>Struts</td>
<td>ams TOF 04-01-01-001 LT</td>
<td>7075-T7351</td>
<td>64</td>
<td>14.60</td>
<td>0.23</td>
<td>1.18</td>
<td>Low risk</td>
<td>Note 2</td>
<td>Page 76, Note 4</td>
</tr>
<tr class="even">
<td>Sensor Boxes Bracket</td>
<td>ams TOF 04-01-008 LT</td>
<td>7075-T7351</td>
<td>64</td>
<td>17.84</td>
<td>0.28</td>
<td>0.79</td>
<td>Low risk</td>
<td>Note 2</td>
<td>Page 76, Note 4</td>
</tr>
<tr class="odd">
<td>Sensor Boxes</td>
<td>ams TOF 02-001 LT</td>
<td>CFRP T300 Fabric</td>
<td><p>115.9</p>
<p>115.9</p>
<p>14.3</p></td>
<td><p>X=-9.7</p>
<p>Y=9.8</p>
<p>XY=3.9</p></td>
<td><p>0.08</p>
<p>0.08</p>
<p>0.27</p></td>
<td>1.56</td>
<td>Low risk</td>
<td>Note 6</td>
<td><p>Page 77, Note 4 Margin</p>
<p>of safety Note 5</p></td>
</tr>
<tr class="even">
<td>Boxes/PMT Support</td>
<td>ams TOF 05-05-001 LT</td>
<td>CFRP T300 Fabric</td>
<td><p>115.9</p>
<p>115.9</p>
<p>14.3</p></td>
<td><p>X=13.9</p>
<p>Y=-17.4</p>
<p>XY=-3.5</p></td>
<td><p>0.12</p>
<p>0.15</p>
<p>.25</p></td>
<td>1.17</td>
<td>Low risk</td>
<td>Note 6</td>
<td>Page 77, Note 4, Margin of safety Note 5</td>
</tr>
<tr class="odd">
<td>Scintillator supports</td>
<td></td>
<td>CFRP T300 Fabric</td>
<td><p>115.9</p>
<p>115.9</p>
<p>14.3</p></td>
<td><p>X=17.4</p>
<p>Y=30.5</p>
<p>XY=5.9</p></td>
<td><p>0.15</p>
<p>0.26</p>
<p>0.41</p></td>
<td>0.12</td>
<td>Low risk</td>
<td>Note 6</td>
<td>Page 77, Note 4, Margin of safety, Note 5</td>
</tr>
<tr class="even">
<td colspan="10"><strong>Fasteners</strong></td>
</tr>
<tr class="odd">
<td>Item</td>
<td>Drawing number</td>
<td>Material and temper</td>
<td>Material allowable stress (ksi)</td>
<td>Applied Load (lbf)</td>
<td>Ratio of applied limit stress to allowable stress</td>
<td>Margin of Safety (ult) FS=1.0</td>
<td>Fracture Classification</td>
<td>Rationale</td>
<td>Comments</td>
</tr>
<tr class="even">
<td>Bracket to ring bolts</td>
<td>Joint 1</td>
<td><p>NAS1351N5</p>
<p>A-286 0.3125-24</p></td>
<td>160</td>
<td>Axial = 617 Shear = 1153</td>
<td>0.75</td>
<td>0.14</td>
<td>Fail-safe</td>
<td>Note 3</td>
<td>Combined tension and shear, Note7</td>
</tr>
<tr class="odd">
<td>USS to Upper bracket bolts</td>
<td>Joint 2</td>
<td><p>NAS1351N6</p>
<p>A-286 0.375-24</p></td>
<td>160</td>
<td>Axial =1177 Shear = 383</td>
<td>0.77</td>
<td>0.16</td>
<td>Fail-safe</td>
<td>Note 3</td>
<td>Total thread shear ultimate, Note 7</td>
</tr>
<tr class="even">
<td>USS to L bracket bolts</td>
<td>Joint 3</td>
<td><p>NAS1351N3</p>
<p>A-286 0.190-32</p></td>
<td>160</td>
<td>Axial = 116 Shear = 248</td>
<td>0.79</td>
<td>0.33</td>
<td>Fail-safe</td>
<td>Note 3</td>
<td>Total thread shear ultimate, Note 7</td>
</tr>
<tr class="odd">
<td>Ring to Honeycomb bolts</td>
<td>Joint 4</td>
<td><p>NAS1351N4</p>
<p>A-286 0.25-28</p></td>
<td>160</td>
<td><p>Axial = 47</p>
<p>Shear = 778</p></td>
<td>0.78</td>
<td>0.26</td>
<td>Fail-safe</td>
<td>Note 3</td>
<td>Total thread shear ultimate, Note 7</td>
</tr>
</tbody>
</table>

Notes:

1\) The components will be classified as per JSC 25863A, August 1998 to
comply with NASA-STD-5003, October 1996 and SSP 30558 Rev. B, June 1994

2\) The component will be classified as fail-safe as per section
5.1.L.1, 5.1.L.2.A and 5.1.L.2.B.3 of JSC 25863 A and will be shown that
the component possesses acceptable durability (possesses acceptable
resistance to crack growth)

3\) The component will be classified as fail-safe as per section 5.1 c
of JSC 25863 A

4\) Ref. Lower Time of Flight (LTOF) Structural Analysis Report,
RICSYS-RP-CGS-012 issue 1, 29 June 2004

5\) Tsai-Hill equation shown in report note 4, page 44. Margin of safety
is (1/ Failure index)-1

6\) The component will be classified as low risk as per sect. 5.2 d of
JSC 25863A.

7\) Ref. AMS-02 Bolt Analysis_Update_v4.(1), 8/4/2005

**Fracture Classification of AMS-02 Ring Imaging Chernekov Counter
(RICH)**

<table>
<colgroup>
<col style="width: 11%" />
<col style="width: 9%" />
<col style="width: 10%" />
<col style="width: 7%" />
<col style="width: 9%" />
<col style="width: 10%" />
<col style="width: 8%" />
<col style="width: 9%" />
<col style="width: 7%" />
<col style="width: 14%" />
</colgroup>
<tbody>
<tr class="odd">
<td>Item</td>
<td>Drawing number</td>
<td>Material and temper</td>
<td>Material allowable stress (ksi)</td>
<td>Max. applied tensile stress (ksi)</td>
<td>Ratio of applied limit stress to allowable stress</td>
<td>Margin of Safety (ult) FS=2.0</td>
<td>Fracture Classification</td>
<td>Rationale</td>
<td>Comments</td>
</tr>
<tr class="even">
<td colspan="10"><strong>External Structure</strong></td>
</tr>
<tr class="odd">
<td>Primary beam</td>
<td></td>
<td>7075-T7351</td>
<td>64</td>
<td>12.7</td>
<td>0.20</td>
<td>1.51</td>
<td>Low risk</td>
<td>Note 2</td>
<td>Page 47, Note 4</td>
</tr>
<tr class="even">
<td>Secondary Internal beam</td>
<td></td>
<td>7075-T7351</td>
<td>64</td>
<td>14.2</td>
<td>0.22</td>
<td>1.26</td>
<td>Low risk</td>
<td>Note 2</td>
<td>Page 47, Note 4</td>
</tr>
<tr class="odd">
<td colspan="10"><strong>Internal Structure</strong></td>
</tr>
<tr class="even">
<td>Structural members</td>
<td>12-RICSYS- 10-001</td>
<td>7075-T7351</td>
<td>64</td>
<td>9.0</td>
<td>0.14</td>
<td>&gt;2.0</td>
<td>Low risk</td>
<td>Note 2</td>
<td>Page 47, Note 4</td>
</tr>
<tr class="odd">
<td>Structural members</td>
<td>12-RICSYS- 20-002</td>
<td>6061-T6</td>
<td>39.5</td>
<td>13.3</td>
<td>0.34</td>
<td>0.48</td>
<td>Low risk</td>
<td>Note 2</td>
<td>Page 47, Note 4</td>
</tr>
<tr class="even">
<td>Reflector Support</td>
<td>12-RICSYS- 40-001</td>
<td>7075-T7351</td>
<td>64</td>
<td>8.20</td>
<td>0.13</td>
<td>&gt;2.0</td>
<td>Low risk</td>
<td>Note 2</td>
<td>Page 47, Note 4</td>
</tr>
<tr class="odd">
<td>Reflector</td>
<td>13-RICSYS- 00-008</td>
<td>CFRP BRYTE EX-1515</td>
<td>68.6, 68.6 27.2</td>
<td>X=2.1, Y=1.9 XY=1.1</td>
<td>0.03, 0.028, 0.04</td>
<td>&gt;2.0</td>
<td>Low risk</td>
<td>Note 5</td>
<td>Page 48, Note 4, Margin of safety, Note 6</td>
</tr>
<tr class="even">
<td colspan="10"><strong>Fasteners</strong></td>
</tr>
<tr class="odd">
<td>Item</td>
<td>Drawing number</td>
<td>Material and temper</td>
<td>Material allowable stress (ksi)</td>
<td>Applied Load (lbf)</td>
<td>Ratio of applied limit stress to allowable yield stress</td>
<td>Margin of Safety (ult) FS=1.0</td>
<td>Fracture Classification</td>
<td>Rationale</td>
<td>Comments</td>
</tr>
<tr class="even">
<td colspan="10">Joint 1</td>
</tr>
<tr class="odd">
<td>External Structure bolts</td>
<td></td>
<td><p>NAS1351N4</p>
<p>A-286, 0.25-28</p></td>
<td>160</td>
<td>Tension = 66 Shear = 946</td>
<td>0.77</td>
<td>0.44</td>
<td>Fail-safe</td>
<td>Note 3</td>
<td>Combined tension and shear, Note 7</td>
</tr>
<tr class="even">
<td colspan="10">Joint 2</td>
</tr>
<tr class="odd">
<td>External to Internal structure bolts</td>
<td></td>
<td>A4-70 0.118-44 (3 mm)</td>
<td>101.5</td>
<td>Tension = 88 Shear = 60</td>
<td>0.87</td>
<td>0.70</td>
<td>Fail-safe</td>
<td>Note 3</td>
<td>Combined tension and shear, Note 7</td>
</tr>
<tr class="even">
<td colspan="10">Joint 3</td>
</tr>
<tr class="odd">
<td>External Structure bolts</td>
<td></td>
<td><p>NAS1351N5</p>
<p>A-286 0.3125-24</p></td>
<td>160</td>
<td>Tension = 486 Shear = 728</td>
<td>0.79</td>
<td>0.10</td>
<td>Fail-safe</td>
<td>Note 3</td>
<td>Combined tension and shear, Note 7</td>
</tr>
</tbody>
</table>

Notes:

1\) The components will be classified as per JSC25863A, August 1998 to
comply with NASA-STD-5003, October 1996 and SSP 30558 Rev. B, June 1994

2\) The component will be classified as low risk as per section 5.1.L.1,
5.1.L.2.A and 5.1.L.2.B.3 of JSC 25863A and will be shown that the
component possesses acceptable durability (Possesses acceptable
resistance to crack growth)

3\) The component will be classified as fail-safe as per section 5.1.c
of JSC 25863A

4\) Ref. RICH Structural Analysis report, RICSYS-RP-CGS-009, issue 1, 29
June 2004

5\) The Component will be classified as low risk as per section 5.2 d of
JSC 25863 A

6\) Tsai-Hill equation shown in report (note 4) page 44. Margin of
safety = (1/ Failure index)-1

7\) Ref. AMS-02 Bolt Analysis_Update_v4.(1), 8/4/2005

**Fracture Classification of AMS-02 Electro Magnetic Calorimeter
(ECAL)**

<table>
<colgroup>
<col style="width: 11%" />
<col style="width: 9%" />
<col style="width: 10%" />
<col style="width: 7%" />
<col style="width: 9%" />
<col style="width: 10%" />
<col style="width: 8%" />
<col style="width: 9%" />
<col style="width: 7%" />
<col style="width: 14%" />
</colgroup>
<tbody>
<tr class="odd">
<td>Item</td>
<td>Drawing number</td>
<td>Material and temper</td>
<td>Material allowable stress (ksi)</td>
<td>Max. applied tensile stress (ksi)</td>
<td>Ratio of applied limit stress to allowable stress</td>
<td>Margin of Safety (ult) FS=1.4</td>
<td>Fracture Classification</td>
<td>Rationale</td>
<td>Comments</td>
</tr>
<tr class="even">
<td>Honeycomb Face plate</td>
<td>ECAL0-10-Je</td>
<td>2024-T4 (2A12-T4)</td>
<td>61</td>
<td>16.0</td>
<td>0.26</td>
<td>1.73</td>
<td>Low risk</td>
<td>Note 2</td>
<td>Page 27, Note 4</td>
</tr>
<tr class="odd">
<td>Honeycomb I frame</td>
<td>ECAL0-11-Je</td>
<td>2014-T6 (2A14-T6)</td>
<td>65.3</td>
<td>21.3</td>
<td>0.33</td>
<td>1.19</td>
<td>Low risk</td>
<td>Note 2</td>
<td>Page 27, Note 4</td>
</tr>
<tr class="even">
<td>Side panels</td>
<td>ECAL0-20-Je ECAL0-30-Je</td>
<td>2014-T6 (2A14-T6)</td>
<td>65.3</td>
<td>21.9</td>
<td>0.34</td>
<td>1.13</td>
<td>Low risk</td>
<td>Note 2</td>
<td>Page 27, Note 4</td>
</tr>
<tr class="odd">
<td>Bracket</td>
<td>ECAL0-41-Je</td>
<td>7050-T7451</td>
<td>69.9</td>
<td>21.0</td>
<td>0.30</td>
<td>1.37</td>
<td>Low risk</td>
<td>Note 2</td>
<td>Page 27, Note 4</td>
</tr>
<tr class="even">
<td>Support beam</td>
<td>ECAL0-42-Je</td>
<td>7050-T7451</td>
<td>69.9</td>
<td>41.2</td>
<td>0.59</td>
<td>0.21</td>
<td>Low risk</td>
<td>Note 2</td>
<td>Page 27, Note 4</td>
</tr>
<tr class="odd">
<td colspan="10"><strong>Fasteners</strong></td>
</tr>
<tr class="even">
<td>Item</td>
<td>Drawing number</td>
<td>Material and temper</td>
<td>Material allowable stress (ksi)</td>
<td>Applied Load (lbf)</td>
<td>Ratio of applied limit stress to allowable yield stress</td>
<td>Margin of Safety (ult) FS=1.0</td>
<td>Fracture Classification</td>
<td>Rationale</td>
<td>Comments</td>
</tr>
<tr class="odd">
<td>Support beam to bracket (Joint 1)</td>
<td>ECAL0-0E</td>
<td>A-286 0.3125-24 NAS 6705U7, 8</td>
<td>160</td>
<td><p>Tensile = 2823</p>
<p>Shear = 0.0</p></td>
<td>0.87</td>
<td>0.334</td>
<td>Fail-safe</td>
<td>Note 3</td>
<td><p>Total thread shear,</p>
<p>Note 5</p></td>
</tr>
<tr class="even">
<td>Bracket to side panels (joint 2)</td>
<td>ECAL0-0E</td>
<td>A-286 0.25-28 NAS 1954C6</td>
<td>180</td>
<td><p>Tensile = 3504</p>
<p>Shear = 216</p></td>
<td>0.91</td>
<td>0.23</td>
<td>Fail-safe</td>
<td>Note 3</td>
<td><p>Total Thread shear,</p>
<p>Note 5</p></td>
</tr>
<tr class="odd">
<td>I Frame to bracket bolts (joint 3)</td>
<td>ECAL0-0E</td>
<td>A-286 0.3125-24, NAS 6705HU10</td>
<td>160</td>
<td></td>
<td></td>
<td></td>
<td>Fail-safe</td>
<td>Note 6</td>
<td>Fail-safe by Engineering Judgment</td>
</tr>
<tr class="even">
<td>I Frame to honeycomb reinforcing and side panels 1 and 2 bolts
(joint4)</td>
<td>ECAL0-0E</td>
<td>A-286 0.0.25-28 NAS1004-2</td>
<td>140</td>
<td></td>
<td></td>
<td></td>
<td>Fail-safe</td>
<td>Note 6</td>
<td>Fail-safe by Engineering Judgment</td>
</tr>
<tr class="odd">
<td>I Frame to side panel 1 bolts(Joint 5)</td>
<td>ECAL0-0E</td>
<td>A-286 0.25-28 NAS1004-9</td>
<td>140</td>
<td></td>
<td></td>
<td></td>
<td>Fail-safe</td>
<td>Note 6</td>
<td>Fail-safe by Engineering Judgment</td>
</tr>
<tr class="even">
<td>I-Frame to side panels 1 and 2 (joint 6)</td>
<td>ECAL0-0E</td>
<td><p>A-286 0.3125-24</p>
<p>NAS1005-1,-2</p></td>
<td>140</td>
<td></td>
<td></td>
<td></td>
<td>Fail-safe</td>
<td>Note 6</td>
<td>Fail-safe by Engineering Judgment</td>
</tr>
<tr class="odd">
<td>I-Frame to honeycomb reinforcing and side panels 1 and 2 (Joint
7)</td>
<td>ECAL0-0E</td>
<td><p>A-286 0.3125-24</p>
<p>NAS1005-1</p></td>
<td>140</td>
<td></td>
<td></td>
<td></td>
<td>Fail-safe</td>
<td>Note 6</td>
<td>Fail-safe by Engineering Judgment</td>
</tr>
<tr class="even">
<td><p>Support to USS</p>
<p>(Joint 8)</p></td>
<td>ECAL0-0E</td>
<td><p>NAS1960C30</p>
<p>A-286 0.625-18</p></td>
<td>140</td>
<td><p>Tensile = 3497</p>
<p>Shear = 4392</p></td>
<td>0.81</td>
<td>0.585</td>
<td>Fail-safe</td>
<td>Note 3</td>
<td>Combined tension and shear, Note 5</td>
</tr>
</tbody>
</table>

Notes:

1\) The components will be classified as per JSC25863A, August 1998 to
comply with NASA-STD-5003, October 1996 and SSP 30558 Rev. B, June 1994.

2\) The component will be classified as low risk as per section 5.1.L.1,
5.1.L.2.A and 5.1.L.2.B.3 of JSC 25863A and will be shown that the
component possesses acceptable durability (Possesses acceptable
resistance to crack growth)

3\) The component will be classified as fail-safe as per section 5.1.c
of JSC 25863A

4\) Flight ECAL Stress Analysis after weight savings, April 7, 2004

5\) Ref. ECAL bolt analysis report ESCG-4450-05-STAN-DOC-0131, February
2006

6\) The components will be classified as fail-safe by Engineering
Judgment as per section 5.1.c of JSC25863A

**Fracture Classification of the AMICA Star Tracker**

<table>
<colgroup>
<col style="width: 9%" />
<col style="width: 9%" />
<col style="width: 9%" />
<col style="width: 9%" />
<col style="width: 9%" />
<col style="width: 9%" />
<col style="width: 9%" />
<col style="width: 9%" />
<col style="width: 9%" />
<col style="width: 12%" />
</colgroup>
<tbody>
<tr class="odd">
<td>Item</td>
<td>Drg. No.</td>
<td>Materials and temper</td>
<td>Material allowable stress (ksi)</td>
<td>Max. limit stress (Ksi)</td>
<td>Limit stress to allowable ratio</td>
<td>M.S. (ult) FS=2.0</td>
<td>Fracture Classification</td>
<td>Rationale</td>
<td>Comments</td>
</tr>
<tr class="even">
<td>Upper bracket</td>
<td></td>
<td>CFRP M55J ACGLTM110</td>
<td>154</td>
<td>43</td>
<td>0.35</td>
<td>0.41</td>
<td>Low risk</td>
<td>Note 4</td>
<td>Page 13, Note 5 Margin of Safety , Note 9</td>
</tr>
<tr class="odd">
<td>Lower bracket</td>
<td></td>
<td>CFRP M55J ACGLTM110</td>
<td>154</td>
<td>31.6</td>
<td>0.45</td>
<td>0.11</td>
<td>Low risk</td>
<td>Note 4</td>
<td>Page 13, Note 5, Margin of Safety , Note 9</td>
</tr>
<tr class="even">
<td>Baffle to M structure bracket</td>
<td></td>
<td>7075-T7351</td>
<td>59</td>
<td>29.2</td>
<td>0.49</td>
<td>0.01</td>
<td>Low risk</td>
<td>Note 2</td>
<td>Page 11, Note 6</td>
</tr>
<tr class="odd">
<td colspan="10"><strong>Fasteners</strong></td>
</tr>
<tr class="even">
<td>Item</td>
<td>Drawing number</td>
<td>Material and temper</td>
<td>Material allowable stress (ksi)</td>
<td>Applied Load (lbf)</td>
<td>Ratio of applied limit stress to allowable stress</td>
<td>Margin of Safety (ult) FS=1.0</td>
<td>Fracture Classification</td>
<td>Rationale</td>
<td>Comments</td>
</tr>
<tr class="odd">
<td>Upper bracket to tracker plane 1 bolts</td>
<td></td>
<td>A286, 0.3937 (M10)</td>
<td>160</td>
<td><p>Tension =103</p>
<p>Shear =498</p></td>
<td>0.63</td>
<td>0.27</td>
<td>Fail-safe</td>
<td>Note 3</td>
<td><p>Total Thread shear,</p>
<p>Note 7, page VI</p></td>
</tr>
<tr class="even">
<td>Upper bracket to lower bracket bolts</td>
<td></td>
<td><p>NAS1351N3</p>
<p>A286, 0.190-32</p></td>
<td>160</td>
<td><p>Tension =163</p>
<p>Shear =154</p></td>
<td>0.89</td>
<td>0.22</td>
<td>Fail- safe</td>
<td>Note 3</td>
<td><p>Total Thread shear,</p>
<p>Note 7, page X</p></td>
</tr>
<tr class="odd">
<td>Lower bracket to tracker conical flange</td>
<td></td>
<td>A286, 0.118 (M3)</td>
<td>160</td>
<td><p>Tension =15</p>
<p>Shear =163</p></td>
<td>0.95</td>
<td>0.61</td>
<td>Fail- safe</td>
<td>Note 3</td>
<td>Combined tension and shear , Note 7, page XIII</td>
</tr>
<tr class="even">
<td>Baffle bracket baffle side to baffle bolts</td>
<td></td>
<td><p>NAS1351N3</p>
<p>A286, 0.190-32</p></td>
<td>160</td>
<td><p>Tension =32</p>
<p>Shear =13</p></td>
<td>0. 87</td>
<td>0.23</td>
<td>Fail-safe</td>
<td>Note 3</td>
<td>Combined tension and shear, Note 8, page 14</td>
</tr>
</tbody>
</table>

Notes:

1\) The components will classified as per JSC 25863A, August 1998 to
comply with NASA-STD-5003, October 1996 and SSP30558 Rev.B, June 1994

2\) The components will be classified as low risk as per sect. 5.1.L.1,
5.1.L.2.A and 5.1.L.2.B.3 of JSC 25863A and will be shown that the
component possesses acceptable durability (Possesses acceptable
resistance to crack growth)

3\) The component will be classified as fail-safe as per sect 5.1.c of
JSC 25863A

4\) The components will be classified as low risk as per section 5.2 d
of JSC 25863A

5\) Ref. AMS-02 AMICA Star Tracker Support Design, Rev 1 INFN Rome, 27
June 2005

6\) Ref. Baffle Support design, INFN Rome, Rev.1 27 June 2005

7\) Ref. ASTS_July2004_Rev1.doc, Appendix 2_ASTS.doc

8\) Ref. Baffle_April2005_Rev1.doc, Appendix1_Baffle.doc

9\) Tsai-Hill equation shown in report note 5, page 12. Margin of safety
= (1/Fsult\*Failure index)-1

**Fracture Classification of AMS-02 Silicon Tracker**

<table>
<colgroup>
<col style="width: 11%" />
<col style="width: 9%" />
<col style="width: 10%" />
<col style="width: 7%" />
<col style="width: 9%" />
<col style="width: 10%" />
<col style="width: 8%" />
<col style="width: 9%" />
<col style="width: 7%" />
<col style="width: 14%" />
</colgroup>
<tbody>
<tr class="odd">
<td>Item</td>
<td>Drawing number</td>
<td>Material and temper</td>
<td>Material allowable stress (ksi)</td>
<td>Max. applied tensile stress (ksi)</td>
<td>Ratio of applied limit stress to allowable stress</td>
<td>Margin of Safety (ult) FS=2.0</td>
<td>Fracture Classification</td>
<td>Rationale</td>
<td>Comments</td>
</tr>
<tr class="even">
<td colspan="10"><strong>Tracker Outer Planes</strong></td>
</tr>
<tr class="odd">
<td>Sandwich facing</td>
<td>AMS II 154 A0 AMS II 155 A0</td>
<td>Carbon fiber M60 J Cyanate Ester</td>
<td>50.7</td>
<td><p>fx=0.536</p>
<p>fy=0.826</p>
<p>fxy=0.276</p></td>
<td>-</td>
<td>&gt;2.0</td>
<td>Low risk</td>
<td>Note 4</td>
<td>Page 22 ,,Note 5</td>
</tr>
<tr class="even">
<td>Sandwich core</td>
<td>AMS II 154 A0 AMS II 155 A0</td>
<td>Hexcel Honeycomb 3/16 in. Al. 5056</td>
<td>0.11</td>
<td>0.004</td>
<td>0.03</td>
<td>16.0</td>
<td>Low risk</td>
<td>Note 4</td>
<td>Page 22, Note 5</td>
</tr>
<tr class="odd">
<td colspan="10"><strong>Tracker Inner Planes</strong></td>
</tr>
<tr class="even">
<td>Sandwich core</td>
<td></td>
<td>Hexcel Honeycomb 3/8 in Al. 5056</td>
<td>0.025</td>
<td>0.011</td>
<td>0.45</td>
<td>0.12</td>
<td>Low risk</td>
<td>Note 4</td>
<td>Page 27, Note 5</td>
</tr>
<tr class="odd">
<td>Sandwich facing</td>
<td></td>
<td>Carbon fiber M60 J Cyanate Ester</td>
<td>72.5</td>
<td><p>fx=4.06</p>
<p>fy=3.33</p>
<p>fxy=1.65</p></td>
<td>-</td>
<td>4.8</td>
<td>Low risk</td>
<td>Note 4</td>
<td>Page 27, Note 5</td>
</tr>
<tr class="even">
<td>Insert ring core</td>
<td></td>
<td>Hexcel Honeycomb 3/16 in. Al. 5056</td>
<td>0.11</td>
<td>0.024</td>
<td>0.22</td>
<td>1.26</td>
<td>Low risk</td>
<td>Note 4</td>
<td>Page 27, Note 5</td>
</tr>
<tr class="odd">
<td>Tracker feet</td>
<td></td>
<td>Ti-6Al-4V</td>
<td>130</td>
<td>56.4</td>
<td>0.43</td>
<td>0.14</td>
<td>Fail-safe</td>
<td>Note 3</td>
<td>Page 5, Note 6</td>
</tr>
<tr class="even">
<td colspan="10"><strong>Fasteners</strong></td>
</tr>
<tr class="odd">
<td>Item</td>
<td>Drawing number</td>
<td>Material and temper</td>
<td>Material allowable stress (ksi)</td>
<td>Applied Load (lbf)</td>
<td>Ratio of applied limit stress to allowable stress</td>
<td>Margin of Safety (ult) FS=1.0</td>
<td>Fracture Classification</td>
<td>Rationale</td>
<td>Comments</td>
</tr>
<tr class="even">
<td>Tracker feet to magnet (Joint1)</td>
<td></td>
<td>A4-70, 0.3125-24 UNF</td>
<td>101.5</td>
<td><p>Tension = 1203</p>
<p>Shear = 0.0</p></td>
<td>0.83</td>
<td>0.09</td>
<td>Fail-safe</td>
<td>Note 3</td>
<td>Joint separation, Note 7</td>
</tr>
<tr class="odd">
<td>Tracker feet to Tracker shell (Joint2)</td>
<td></td>
<td>A-286 10-32 UNF</td>
<td>200</td>
<td><p>Tension = 2107</p>
<p>Shear = 0.0</p></td>
<td>0.89</td>
<td>0.06</td>
<td>Fail-safe</td>
<td>Note 3</td>
<td>Combined shear and tension, Note 7 Negative M.S. on joint separation
acceptable for fail-safe</td>
</tr>
<tr class="even">
<td>Conical Flange to tracker shell (Joint3)</td>
<td></td>
<td>A-286, M4x33</td>
<td>200</td>
<td><p>Tension = 327</p>
<p>Shear = 333</p></td>
<td></td>
<td></td>
<td>Fail-safe</td>
<td>Note 8</td>
<td>Fail-safe by Engineering Judgment</td>
</tr>
<tr class="odd">
<td>Tracker shell to tracker shell (Joint 4)</td>
<td></td>
<td>A4-70, 0.138-32 UNF</td>
<td>101.5</td>
<td><p>Tension = 59</p>
<p>Shear = 0.0</p></td>
<td></td>
<td></td>
<td>Fail-safe</td>
<td>Note 8</td>
<td>Fail-safe by Engineering Judgment</td>
</tr>
<tr class="even">
<td>Inner plane to tracker shell (Joint 5)</td>
<td></td>
<td>A4-70, M4x12</td>
<td>101.5</td>
<td><p>Tension = 49</p>
<p>Shear = 60</p></td>
<td></td>
<td></td>
<td>Fail-safe</td>
<td>Note 8</td>
<td>Fail-safe by Engineering Judgment</td>
</tr>
<tr class="odd">
<td>Outer plane to conical flange (Joint 6)</td>
<td></td>
<td>A4-70, M4x40</td>
<td>101.5</td>
<td><p>Tension = 29</p>
<p>Shear = 80</p></td>
<td></td>
<td></td>
<td>Fail-safe</td>
<td>Note 8</td>
<td>Fail-safe by Engineering Judgment</td>
</tr>
<tr class="even">
<td>Outer plane to conical flange (Joint 7)</td>
<td></td>
<td>A4-70, M4x40</td>
<td>101.5</td>
<td><p>Tension = 29</p>
<p>Shear = 80</p></td>
<td></td>
<td></td>
<td>Fail-safe</td>
<td>Note 8</td>
<td>Fail-safe by Engineering Judgment</td>
</tr>
</tbody>
</table>

Notes:

1\) The components will be classified as per JSC25863A, August 1998 to
comply with NASA-STD-5003, October 1996 and SSP 30558 Rev. B, June 1994.

2\) The component will be classified as low risk as per section 5.1.L.1,
5.1.L.2.A and 5.1.L.2.B.3 of JSC 25863A and will be shown that the
component possesses acceptable durability (Possesses acceptable
resistance to crack growth)

3\) The component will be classified as fail-safe as per section 5.1.c
of JSC 25863A

4\) The component will be classified as low risk as per section 5.2d of
JSC 25863A

5\) Ref. AMS Silicon Tracker Support Plates Analysis Report Extension
AMS-ANR-002, Contraves Space, 19 November 1999.

6\) Ref. AMS 02 Tracker Support Feet , Rev. 1 Structural Verification
Document, ISATEC, 16 June 2004

7\) AMS Tracker bolt analysis compliance with NSTS 08307 standards,
University of Geneva Memo, 26 January, 2006

8\) There are multiple fasteners in this joint and the fasteners are
classified as fail-safe by Engineering Judgment as per 5.1.c of JSC
25863A

**Fracture Classification for AMS-02 Cryomagnet**

<table>
<colgroup>
<col style="width: 11%" />
<col style="width: 9%" />
<col style="width: 10%" />
<col style="width: 7%" />
<col style="width: 9%" />
<col style="width: 10%" />
<col style="width: 8%" />
<col style="width: 9%" />
<col style="width: 7%" />
<col style="width: 14%" />
</colgroup>
<tbody>
<tr class="odd">
<td>Item</td>
<td>Drawing Number</td>
<td>Material and temper</td>
<td>Material allowable stress (ksi)</td>
<td>Max. applied tensile stress (ksi)</td>
<td>Ratio of applied limit stress to allowable stress</td>
<td>Margin of Safety (ult) FS =1.50</td>
<td>Fracture Classification</td>
<td>Rationale</td>
<td>Comments</td>
</tr>
<tr class="even">
<td>Race track End frame</td>
<td>SCD0825</td>
<td><p>6061-T6 (10 in)</p>
<p>1.8 K</p></td>
<td>53.7</td>
<td>29.4</td>
<td>0.55</td>
<td>0.22</td>
<td>Low risk</td>
<td>Note 2</td>
<td><p>Page 7, sect.1.1.1</p>
<p>Note 4</p></td>
</tr>
<tr class="odd">
<td>Dipole Island</td>
<td>SCD0810</td>
<td><p>6061-T6 (10 in)</p>
<p>1.8 K</p></td>
<td>53.7</td>
<td>29.0</td>
<td>0.54</td>
<td>0.23</td>
<td>Low risk</td>
<td>Note 2</td>
<td><p>Page 8, sect.1.1.2 c</p>
<p>Note 4</p></td>
</tr>
<tr class="even">
<td>Race track coils</td>
<td>SCD0841</td>
<td><p>6061-T6 (10 in)</p>
<p>1.8 K</p></td>
<td>53.7</td>
<td>19.6</td>
<td>0.37</td>
<td>0.83</td>
<td>Low risk</td>
<td>Note 2</td>
<td><p>Page 8,sect.1.1.2 b</p>
<p>Note 4</p></td>
</tr>
<tr class="odd">
<td>Race track edge plate outer</td>
<td>SCD0851-4</td>
<td><p>2219-T851</p>
<p>300 K</p></td>
<td>60.9</td>
<td>27.6</td>
<td>0.45</td>
<td>0.47</td>
<td>Low risk</td>
<td>Note 2</td>
<td>Page 13, sect 1.1.5 a, max. tens stress preload warm, Note 4</td>
</tr>
<tr class="even">
<td>Race track edge plate curved</td>
<td>SCD0851-3</td>
<td><p>6061-T6 (10 in)</p>
<p>300 K</p></td>
<td>36.9</td>
<td>21.6</td>
<td>0.58</td>
<td>0.14</td>
<td>Low risk</td>
<td>Note 2</td>
<td>Page 13, sect 1.1.5 b, max. tens stress preload warm, Note 4</td>
</tr>
<tr class="odd">
<td>Dipole edge Plate</td>
<td>SCD0812-01</td>
<td><p>6061-T6 (10 in)</p>
<p>300 K</p></td>
<td>36.9</td>
<td>22.5</td>
<td>0.61</td>
<td>0.10</td>
<td>Low risk</td>
<td>Note 2</td>
<td>Page 14, sect 1.1.5 c, max. tens stress preload warm, Note 4</td>
</tr>
<tr class="even">
<td>Helium vessel Fx support pin</td>
<td>SCD0889-02</td>
<td><p>316 Hi proof stainless steel</p>
<p>4 K</p></td>
<td>232.1</td>
<td>143.6</td>
<td>0.62</td>
<td>0.08</td>
<td>Low risk</td>
<td>Note 2</td>
<td>Page 48, sect 4.1.d inertia loads, Note 4</td>
</tr>
<tr class="odd">
<td>Helium vessel Fy support pin</td>
<td>SCD0910-01</td>
<td><p>316 Hi proof stainless steel</p>
<p>4 K</p></td>
<td>31.9</td>
<td>20.5</td>
<td>0.64</td>
<td>0.42 yield</td>
<td>Low risk</td>
<td>Note 2</td>
<td>Page 49, sect 4.2.A inertia loads, Note 4</td>
</tr>
<tr class="even">
<td>Helium vessel Fz support pin</td>
<td>SCD0898-01</td>
<td><p>316 Hi proof stainless steel</p>
<p>4 K</p></td>
<td>232.1</td>
<td>130.7</td>
<td>0.56</td>
<td>0.18</td>
<td>Low risk</td>
<td>Note 2</td>
<td>Page 54, sect 4.4.C inertia loads, Note 4</td>
</tr>
<tr class="odd">
<td colspan="10"><strong>Fasteners</strong></td>
</tr>
<tr class="even">
<td>Item</td>
<td>Drawing Number</td>
<td>Material and temper</td>
<td>Material allowable Load (lbf)</td>
<td>Applied bolt limit Load (lbf)</td>
<td>Ratio of applied limit load to allowable load</td>
<td>Margin of Safety FS =1.0</td>
<td>Fracture Classification</td>
<td>Rationale</td>
<td>Comments</td>
</tr>
<tr class="odd">
<td>Dipole crossbeam to dipole edge plate</td>
<td>SCD0824</td>
<td>M6 316 Hi proof stainless steel</td>
<td>7229 (cold)</td>
<td>2779</td>
<td>0.47</td>
<td>1.26</td>
<td>Fail-safe</td>
<td>Note 3</td>
<td>Appendix 7, page 2, Note 4</td>
</tr>
<tr class="even">
<td>Dipole crossbeam to dipole island</td>
<td>SCD0824</td>
<td>M6 316 Hi proof stainless steel</td>
<td>3976 (warm)</td>
<td>767</td>
<td>0.23</td>
<td>3.50</td>
<td>Fail-safe</td>
<td>Note 3</td>
<td>Appendix 7, page 2, Note 4</td>
</tr>
<tr class="odd">
<td>Dipole crossbeam to RTEF bolts</td>
<td>SCD0824</td>
<td>M5, 316 Hi proof stainless steel</td>
<td>5107 (cold)</td>
<td>3294</td>
<td>0.79</td>
<td>0.35</td>
<td>Fail-safe</td>
<td>Note 3</td>
<td><p>Appendix 7, Page 3,</p>
<p>Note 4</p></td>
</tr>
<tr class="even">
<td>Dipole island to RTEF bolts</td>
<td>SCD0824</td>
<td>M5, 316 Hi proof stainless steel</td>
<td>2809 (warm)</td>
<td>868</td>
<td>0.37</td>
<td>1.81</td>
<td>Fail- safe</td>
<td>Note 3</td>
<td><p>Appendix 7, Page 3,</p>
<p>Note 4</p></td>
</tr>
<tr class="odd">
<td>Dipole leaf spring to RTEF</td>
<td>SCD0824</td>
<td>M5, 316 Hi proof stainless steel</td>
<td>2809 (warm)</td>
<td>694</td>
<td>0.29</td>
<td>2.51</td>
<td>Fail- safe</td>
<td>Note 3</td>
<td><p>Appendix 7, page 5</p>
<p>Note 4</p></td>
</tr>
<tr class="even">
<td>Helium vessel Fz support bolts</td>
<td>SCD0898</td>
<td>M8, 316 Hi proof stainless steel</td>
<td>232 ksi)</td>
<td>159.5</td>
<td>0.84</td>
<td>0.26</td>
<td>Fail- safe</td>
<td>Note 3</td>
<td><p>Appendix 7, Page 6</p>
<p>Note 4</p></td>
</tr>
</tbody>
</table>

Notes:

1\) The components will be classified as per JSC 25863A, August 1998 to
comply with NASA-STD-5003, October 1996 and SSP 30558 Rev. B, June 1994

2\) The component will be classified as low risk as per section 5.1.L.1,
5.1.L.2.A and 5.1.L.2.B.3 of JSC25863A, and will be shown that the
component possesses acceptable durability(Possesses acceptable
resistance to crack growth)

3\) The component will be classified fail-safe as per section 5.1.c of
JSC25853A

4\) Reference summary of Structural Analysis of AMS-02 Super conducting
Magnet, September 2003, issue 02

5\) The component will be classified fail-safe by Engineering Judgment
as per section 5.1.c of JSC25853A

**Fracture Classification of AMS-02 Helium Tank**

<table>
<colgroup>
<col style="width: 11%" />
<col style="width: 9%" />
<col style="width: 10%" />
<col style="width: 7%" />
<col style="width: 9%" />
<col style="width: 10%" />
<col style="width: 8%" />
<col style="width: 9%" />
<col style="width: 7%" />
<col style="width: 14%" />
</colgroup>
<tbody>
<tr class="odd">
<td>Item</td>
<td>Drawing number</td>
<td>Material and temper</td>
<td>Material allowable yield stress (ksi)</td>
<td>Max. applied yield stress (ksi)</td>
<td>Ratio of applied stress to allowable stress</td>
<td>Margin of Safety (ult) FS=2.0</td>
<td>Fracture Classification</td>
<td>Rationale</td>
<td>Comments</td>
</tr>
<tr class="even">
<td>Central Ring</td>
<td>SCD 0905-01</td>
<td>5083-H111 forging</td>
<td>26.49</td>
<td>21.19</td>
<td>0.80</td>
<td><p>0.0003</p>
<p>( bearing yield)</p></td>
<td>Non Fracture critical</td>
<td>Note 2</td>
<td>Page 3-7, Note 3</td>
</tr>
<tr class="odd">
<td>Thru tube</td>
<td>SCD 0903-01 SCD 0902-01</td>
<td>5083-H321 cold worked forging</td>
<td>35.67</td>
<td>27.24</td>
<td>0.76</td>
<td>0.05(yield)</td>
<td>Non Fracture critical</td>
<td>Note 2</td>
<td>Page 3-12, Note 3</td>
</tr>
<tr class="even">
<td>Outer ring weld</td>
<td>SCD 0905-02,-03</td>
<td>5083-H321</td>
<td>22.09</td>
<td>5.16</td>
<td>0.23</td>
<td>2.42(yield)</td>
<td>Non Fracture critical</td>
<td>Note 2</td>
<td>Page3-19, Note 3</td>
</tr>
<tr class="odd">
<td>Inner ring weld</td>
<td>SCD 0905-04,-05</td>
<td>5083-H321</td>
<td>23.46</td>
<td>20.3</td>
<td>0.86</td>
<td>0.69(yield)</td>
<td>Non Fracture critical</td>
<td>Note 2</td>
<td>Page 3-16, Note 3</td>
</tr>
<tr class="even">
<td>Central plate weld</td>
<td>SCD0905-01</td>
<td>5083-321</td>
<td>25.2</td>
<td>16.71</td>
<td>0.66</td>
<td>0.21 (yield)</td>
<td>Non Fracture critical</td>
<td>Note 2</td>
<td>Page 3-35, Note 3</td>
</tr>
<tr class="odd">
<td>Central Ring weld</td>
<td>SCD0905-01</td>
<td>5083-H111 forging</td>
<td>25.2</td>
<td>16.0</td>
<td>0.63</td>
<td>0.26 (yield0</td>
<td>Non Fracture critical</td>
<td>Note 2</td>
<td>Page 3-7, Note 3</td>
</tr>
</tbody>
</table>

Notes:

1\) The components will be classified as per JSC25863A, August 1998 to
comply with NASA-STD-5003, October 1996 and SSP 30558 Rev. B, June 1994.

2\) The component will be classified as non fracture critical
(Leak-before burst) as per sect.5.1 d of JSC 25863 A

3\) Ref. Helium tank strength and stability assessment, October 24, 2006

**Fracture Classification for AMS-02 Cryomagnet Suspension Straps**

<table>
<colgroup>
<col style="width: 11%" />
<col style="width: 9%" />
<col style="width: 10%" />
<col style="width: 7%" />
<col style="width: 9%" />
<col style="width: 10%" />
<col style="width: 8%" />
<col style="width: 9%" />
<col style="width: 7%" />
<col style="width: 14%" />
</colgroup>
<tbody>
<tr class="odd">
<td>Item</td>
<td>Drawing Number</td>
<td>Material and temper</td>
<td>Material allowable stress (ksi)</td>
<td>Max. applied tensile stress (ksi)</td>
<td>Ratio of applied Ratio of limit stress to allowable stress</td>
<td>Margin of Safety (ult) FS =1.40</td>
<td>Fracture Classification</td>
<td>Rationale</td>
<td>Comments</td>
</tr>
<tr class="even">
<td>Race track end frame clevis C1W1</td>
<td>SCD0825</td>
<td>6061-T6 (10 in)</td>
<td>37.0</td>
<td><p>20087 lbs (axial)</p>
<p>13986 lbs</p>
<p>(transverse)</p></td>
<td><p>6503 lbs (axial)</p>
<p>6995 lbs</p>
<p>(transverse)</p></td>
<td>0.109</td>
<td>Fracture critical</td>
<td>Note 2,3</td>
<td>Page 7, Note 5</td>
</tr>
<tr class="odd">
<td>Race track end frame clevis pin C1W1</td>
<td>SCD 0678-02</td>
<td>316L Hi-Proof stainless steel</td>
<td>127.64</td>
<td>85.77</td>
<td>0.67</td>
<td>0.063</td>
<td>Fracture critical</td>
<td>Note 2,3</td>
<td>Page 13, Note 5</td>
</tr>
<tr class="even">
<td>Carbon Band</td>
<td>SCD 0678-03</td>
<td>Carbon Fiber epoxy</td>
<td>275.65</td>
<td>117.7</td>
<td>0.43</td>
<td>0.67</td>
<td>Fracture critical</td>
<td>Note 2,3</td>
<td>Note 4</td>
</tr>
<tr class="odd">
<td>FGR Band</td>
<td>SCD 0678-12</td>
<td>FGR3 epoxy</td>
<td>261.07</td>
<td>59.32</td>
<td>0.22</td>
<td>2.14</td>
<td>Fracture critical</td>
<td>Note 2,3</td>
<td>Note 4</td>
</tr>
<tr class="even">
<td>Glass Band</td>
<td>SCD 0678-11</td>
<td>S2 glass epoxy</td>
<td>217.56</td>
<td>61.22</td>
<td>0.28</td>
<td>1.53</td>
<td>Fracture critical</td>
<td>Note 2,3</td>
<td>Note 4</td>
</tr>
<tr class="odd">
<td>Glass Bod</td>
<td>SCD 0678-18</td>
<td>S2 glass epoxy</td>
<td>217.56</td>
<td>98.38</td>
<td>0.45</td>
<td>0.58</td>
<td>Fracture critical</td>
<td>Note 2,3</td>
<td>Note 4</td>
</tr>
</tbody>
</table>

Notes:

1\) The components will be classified as per JSC25863A, August 1998 to
comply with NASA-STD-5003, October 1996 and SSP 30558 Rev. B, June 1994

2\) The component is classified as fracture critical as per sect 5.2 and
is shown acceptable by sect. 6.0 of JSC 25863A

3\) The flight hardware will be tested to a minimum of 1.2 times limit
load

4\) Ref. Space Cryomagnetics Ltd (SCL) analysis, Fax No.1169, 6 March
2002

5\) Ref. Cryomagnet Suspension Strap Analysis, Lockheed Martin, April
2002

**Fracture Classification of Anti Coincidence Counter (ACC)**

<table>
<colgroup>
<col style="width: 11%" />
<col style="width: 9%" />
<col style="width: 10%" />
<col style="width: 7%" />
<col style="width: 9%" />
<col style="width: 10%" />
<col style="width: 8%" />
<col style="width: 9%" />
<col style="width: 7%" />
<col style="width: 14%" />
</colgroup>
<tbody>
<tr class="odd">
<td>Item</td>
<td>Drawing Number</td>
<td>Material and temper</td>
<td>Material allowable stress (ksi)</td>
<td>Max. applied tensile stress (ksi)</td>
<td>Ratio of applied limit stress to allowable stress</td>
<td>Margin of Safety (ult) FS = 2.0</td>
<td>Fracture Classification</td>
<td>Rationale</td>
<td>Comments</td>
</tr>
<tr class="even">
<td>ACC Clamps</td>
<td>ams-02-03 1024</td>
<td>7075-T7351</td>
<td>56</td>
<td>25.8</td>
<td>0.46</td>
<td>0.09</td>
<td>Low risk</td>
<td>Note 2</td>
<td>Page 13, Note 4</td>
</tr>
<tr class="odd">
<td>ACC cylinder</td>
<td>ams-02 1626</td>
<td>CFRP Tenax J UMS2526</td>
<td>211</td>
<td>0.074</td>
<td>0.0004</td>
<td>&gt;2.0</td>
<td>Contained</td>
<td>Note 5</td>
<td></td>
</tr>
<tr class="even">
<td>ACC panels</td>
<td>ams-02 1771c</td>
<td>Bicron BC 414 Polyvinyl Toluene</td>
<td>4.5</td>
<td>0.22</td>
<td>0.049</td>
<td>&gt;2.0</td>
<td>Contained</td>
<td>Note 5</td>
<td></td>
</tr>
<tr class="odd">
<td>Connector support</td>
<td>1812/60- 0004_I_VI</td>
<td>7075-T7351</td>
<td>68</td>
<td>22</td>
<td>0.32</td>
<td>0.54</td>
<td>Low risk</td>
<td>Note 2</td>
<td>Page 17, Note 8</td>
</tr>
<tr class="even">
<td>ACC PMT Support</td>
<td>1812/60- 001_I_VI</td>
<td>7075-T7351</td>
<td>67</td>
<td>0.13</td>
<td>0.002</td>
<td>&gt;2.0</td>
<td>Low risk</td>
<td>Note 2</td>
<td>Note 4</td>
</tr>
<tr class="odd">
<td colspan="10"><strong>Fasteners</strong></td>
</tr>
<tr class="even">
<td>Item</td>
<td>Drawing Number</td>
<td>Material and temper</td>
<td>Material allowable stress (ksi)</td>
<td>Max. applied Load (lbf)</td>
<td>Ratio of applied limit stress to allowable yield stress</td>
<td><p>Margin of Safety (ult)</p>
<p>FS =1.0</p></td>
<td>Fracture Classification</td>
<td>Rationale</td>
<td>Comments</td>
</tr>
<tr class="odd">
<td>ACC clamps to VC flange bolts</td>
<td></td>
<td>A-286 0.190-32</td>
<td>200</td>
<td>Tension = 1091 Shear = 0</td>
<td>0.90</td>
<td>0.06</td>
<td>Fail-safe</td>
<td>Note 3</td>
<td>Joint separation, Note 6</td>
</tr>
<tr class="even">
<td>PMT support to Vacuum case</td>
<td></td>
<td>A-286 0.190-32</td>
<td>160</td>
<td><p>Tension =333</p>
<p>Shear = 143</p></td>
<td>0.88</td>
<td>0.36</td>
<td>Fail-safe</td>
<td>Note 3</td>
<td>Combined tension and shear, note 7</td>
</tr>
</tbody>
</table>

Notes:

1\) The components will be classified as per JSC25863A, August 1998 to
comply with NASA-STD-5003, October 1996 and SSP 30558 Rev. B, June 1994

2\) The component will be classified as low risk as per section 5.1.L.1,
5.1.L.2.A and 5.1.L.2.B.3 of JSC25863A, and will be shown that the
component possesses acceptable durability (Possesses acceptable
resistance to crack growth)

3\) The component will be classified as fail-safe as per section 5.1.c
of JSC 25863A

4\) Ref. AMS-02 Anti Coincidence Counter Structural Verification
Document, Rev. 1, ISATEC, 9 December 2004

5\) The component is classified as contained as per sect. 5.1 g of JSC
25863A

6\) ACC- clamps Mathcad analysis 7/15/2005

7\) PMT-Support Mathcad analysis 7/15/2005

8\) Ref. ACC Connector Support, Documentation of Margin of Safety, 8
March 2007

**Fracture Classification for Zenith Radiator**

<table>
<colgroup>
<col style="width: 11%" />
<col style="width: 9%" />
<col style="width: 10%" />
<col style="width: 7%" />
<col style="width: 9%" />
<col style="width: 10%" />
<col style="width: 8%" />
<col style="width: 9%" />
<col style="width: 7%" />
<col style="width: 14%" />
</colgroup>
<tbody>
<tr class="odd">
<td>Item</td>
<td>Drawing Number</td>
<td>Material and temper</td>
<td>Material allowable stress (ksi)</td>
<td>Max. applied tensile stress (ksi)</td>
<td>Ratio of applied limit stress to allowable stress</td>
<td>Margin of Safety (ult) FS =2.0</td>
<td>Fracture Classification</td>
<td>Rationale</td>
<td>Comments</td>
</tr>
<tr class="even">
<td>Radiator panels</td>
<td>AMS-01.10. 10.000</td>
<td>Rohacell core 2024-T81 face sheets</td>
<td>0.100</td>
<td>0.0497</td>
<td>0.49</td>
<td>0.01</td>
<td>Low risk</td>
<td>Note 5</td>
<td>Page 52, EVA load case Note 4</td>
</tr>
<tr class="odd">
<td>3W interface bracket</td>
<td>AMS-01.00. 00.002</td>
<td>7075-T7351</td>
<td>59.9</td>
<td>26.7</td>
<td>0.45</td>
<td>0.12</td>
<td>Low risk</td>
<td>Note 2</td>
<td>Page 43, Liftoff/landing cases Note 4</td>
</tr>
<tr class="even">
<td>Interface Spokes</td>
<td>AMS-01.30. 00.003</td>
<td>Carbon fiber</td>
<td>87</td>
<td>35.4</td>
<td>0.41</td>
<td>0.23</td>
<td>Low risk</td>
<td>Note 5</td>
<td><p>Page 63, Thermal induced load cases,</p>
<p>Note 4</p></td>
</tr>
<tr class="odd">
<td colspan="10"><strong>Fasteners</strong></td>
</tr>
<tr class="even">
<td>Item</td>
<td>Drawing Number</td>
<td>Material and temper</td>
<td>Material allowable Load (ksi)</td>
<td>Applied Load (lbf)</td>
<td>Ratio of applied limit stress to allowable stress</td>
<td>Margin of Safety FS =1.0</td>
<td>Fracture Classification</td>
<td>Rationale</td>
<td>Comments</td>
</tr>
<tr class="odd">
<td>Sandwich panel to 3w-IF bracket</td>
<td>Joint 0203</td>
<td>A286 0.190-32</td>
<td>160</td>
<td>tension = 28 shear = 300</td>
<td>0.67</td>
<td>0.45</td>
<td>fail-safe</td>
<td>Note 3</td>
<td>Page 98, Note 4</td>
</tr>
<tr class="even">
<td>3w-IF bracket toTRD</td>
<td>Joint 0305</td>
<td>A286 0.25-28</td>
<td>160</td>
<td><p>tension 509</p>
<p>shear = 581</p></td>
<td>0.65</td>
<td>0.42</td>
<td>fail-safe</td>
<td>Note 3</td>
<td>Page 98, Note 4</td>
</tr>
<tr class="odd">
<td>Z bracket to TRD upper plate</td>
<td>Joint 0405</td>
<td>A286 0.190-32</td>
<td>160</td>
<td><p>tension=227</p>
<p>shear = 161</p></td>
<td>0.69</td>
<td>0.53</td>
<td>fail-safe</td>
<td>Note 3</td>
<td>Page 98, Note 4</td>
</tr>
</tbody>
</table>

Notes:

1\) The components will be classified as per JSC25863A, August 1998 to
comply with NASA-STD-5003, October 1996 and SSP 30558 Rev. B, June 1994

2\) The component will be classified as low risk as per section 5.1.L.1,
5.1.L.2.A and 5.1.L.2.B.3 of JSC25863A, and will be shown that the
component possesses acceptable durability( Possesses acceptable
resistance to crack growth)

3\) The component will be classified as fail-safe as per section 5.1.c
of JSC 25863A

4\) Ref. Zenith Radiator Structural analysis Report, AMS-OHB-SAR-001,
issue 4, April 1,2005

5\) The component will be classified as low risk as per section 5.2 d of
JSC 25863A

**Fracture Classification for Main and Tracker Radiator**

<table>
<colgroup>
<col style="width: 11%" />
<col style="width: 9%" />
<col style="width: 10%" />
<col style="width: 7%" />
<col style="width: 9%" />
<col style="width: 10%" />
<col style="width: 8%" />
<col style="width: 9%" />
<col style="width: 7%" />
<col style="width: 14%" />
</colgroup>
<tbody>
<tr class="odd">
<td>Item</td>
<td>Drawing Number</td>
<td>Material and temper</td>
<td>Material allowable stress (ksi)</td>
<td>Max. applied tensile stress (ksi)</td>
<td>Ratio of applied limit stress to allowable stress</td>
<td>Margin of Safety (ult) FS. =2.0</td>
<td>Fracture Classification</td>
<td>Rationale</td>
<td>Comments</td>
</tr>
<tr class="even">
<td>Main radiator panel heat pipes</td>
<td>21-AMS-000.00.XY &amp;22-AMS-000.00.XY</td>
<td>6063-T5</td>
<td>25.35</td>
<td>7.7</td>
<td>0.30</td>
<td>0.54</td>
<td>Low risk</td>
<td>Note 2</td>
<td><p>Pages 189 – 191,</p>
<p>Note 4.</p></td>
</tr>
<tr class="odd">
<td>Tracker radiator panel heat pipes</td>
<td>25-AMS-000.00.XY</td>
<td>6063-T5</td>
<td>25.35</td>
<td>12.82</td>
<td>0.50</td>
<td>0.39</td>
<td>Low risk</td>
<td>Note 2</td>
<td><p>Pages 192-195,</p>
<p>Note 4</p></td>
</tr>
<tr class="even">
<td>Main/Tracker radiator bracket</td>
<td>24-AMS-330.08 .XY</td>
<td>7075-T73</td>
<td>62.97</td>
<td>27.46</td>
<td>0.44</td>
<td>0.15</td>
<td>Low risk</td>
<td>Note 2</td>
<td>Page 198, Note 4</td>
</tr>
<tr class="odd">
<td>Tracker radiator rod 4</td>
<td></td>
<td>Carbon fiber</td>
<td>1022 lbf</td>
<td>266 lbf</td>
<td>0.26</td>
<td>0.92</td>
<td>Low risk</td>
<td>Note 2</td>
<td><p>Pages 188 &amp; 197</p>
<p>Note 4</p></td>
</tr>
<tr class="even">
<td>Main Radiator Skin</td>
<td>21_AMS-000.00.XY, 22-AMS-000.00.XY</td>
<td>2024-T81</td>
<td>62.97</td>
<td>17.68</td>
<td>0.28</td>
<td>0.78</td>
<td>Low risk</td>
<td>Note 2</td>
<td>Page 196, Note 4</td>
</tr>
<tr class="odd">
<td>Tracker radiator skin</td>
<td>25-AMS-000.00 .01, 25-AMS-000.00.02</td>
<td>2024-T81</td>
<td>62.97</td>
<td>27.63</td>
<td>0.44</td>
<td>0.14</td>
<td>Low risk</td>
<td>Note 2</td>
<td>Page 197, Note 4</td>
</tr>
<tr class="even">
<td colspan="10"><strong>Fasteners</strong></td>
</tr>
<tr class="odd">
<td>Item</td>
<td>Drawing Number</td>
<td>Material and temper</td>
<td>Material allowable Load (ksi)</td>
<td>Max. applied Load (lbf)</td>
<td>Ratio of applied limit stress to allowable yield stress</td>
<td>Margin of Safety (ult) FS =1.0</td>
<td>Fracture Classification</td>
<td>Rationale</td>
<td>Comments</td>
</tr>
<tr class="even">
<td>USS to Tracker Radiator I/F brackets</td>
<td>Joint 7</td>
<td><p>A 286 0.250-28</p>
<p>NAS1351 N4</p></td>
<td>160</td>
<td>Tension = 154 Shear = 420</td>
<td>0.66</td>
<td>0.60</td>
<td>fail-safe</td>
<td>Note 3</td>
<td>Page 337, Note 4</td>
</tr>
<tr class="odd">
<td>Tracker radiator panel to I/F brackets</td>
<td>Joint 8</td>
<td>A 286 0.190-32 NAS1351N3</td>
<td>160</td>
<td><p>Tension = 21</p>
<p>Shear = 74</p></td>
<td>0.64</td>
<td>0.80</td>
<td>fail-safe</td>
<td>Note 3</td>
<td>Page 338, note 4</td>
</tr>
<tr class="even">
<td>Tracker radiator panel to condenser plate</td>
<td>Joint 9</td>
<td><p>MS51957</p>
<p>0.138-32</p></td>
<td>80</td>
<td>Tension = 13 Shear = 115</td>
<td>0.75</td>
<td>0.70</td>
<td>fail-safe</td>
<td>Note 3</td>
<td>Page 339, Note 4</td>
</tr>
<tr class="odd">
<td>Main to tracker radiator bracket</td>
<td>Joint 11a</td>
<td><p>A 286 0.190-32</p>
<p>NAS1351N3</p></td>
<td>160</td>
<td>Tension = 16 Shear = 303</td>
<td>0.62</td>
<td>0.66</td>
<td>fail- safe</td>
<td>Note 3</td>
<td>Page 340, Note 4</td>
</tr>
</tbody>
</table>

  -------- ------- ------- ----- ------- ------- ------ ------ ----- ----------
                                                                     

                                                                     

                                                                     

                                                                     

                                                                     

                                                                     

                                                                     

                                                                     

                                                                     

                                                                     

                                                                     

                                                                     
  -------- ------- ------- ----- ------- ------- ------ ------ ----- ----------

Notes:

1\) The components will be classified as per JSC25863A, August 1998 to
comply with NASA-STD-5003, October 1996 and SSP 30558 Rev. B, June 1994

2\) The component will be classified as low risk as per section 5.1.L.1,
5.1.L.2.A and 5.1.L.2.B.3 of JSC25863A, and will be shown that the
component possesses acceptable durability(Possesses acceptable
resistance to crack growth)

3\) The component will be classified as fail-safe as per section 5.1.c
of JSC 25863A

4\) Ref. Main Radiators Structural Analysis Report AMS-02-RP-CGS-005,
issue 4, April 5, 2007

  -------- ------- ------- ----- ------- ------- ------ ------ ----- ----------
                                                                     

                                                                     

                                                                     

                                                                     

                                                                     

                                                                     

                                                                     

                                                                     

                                                                     

                                                                     

                                                                     

                                                                     

                                                                     

                                                                     

                                                                     

                                                                     
  -------- ------- ------- ----- ------- ------- ------ ------ ----- ----------

<table>
<colgroup>
<col style="width: 11%" />
<col style="width: 9%" />
<col style="width: 10%" />
<col style="width: 7%" />
<col style="width: 9%" />
<col style="width: 10%" />
<col style="width: 8%" />
<col style="width: 9%" />
<col style="width: 7%" />
<col style="width: 14%" />
</colgroup>
<tbody>
<tr class="odd">
<td>Item</td>
<td>Drawing Number</td>
<td>Material and temper</td>
<td>Material allowable stress (ksi)</td>
<td>Max. applied tensile stress (ksi)</td>
<td>Ratio of applied limit stress to. allowable stress</td>
<td>Margin of Safety (ult) FS =2.0</td>
<td>Fracture Classification</td>
<td>Rationale</td>
<td>Comments</td>
</tr>
<tr class="even">
<td>XPD structure</td>
<td>24- AMS- 120.AB.XY</td>
<td>7075-T7351</td>
<td>58.29</td>
<td>26.73</td>
<td>0.46</td>
<td>0.09</td>
<td>Low risk</td>
<td>Note 2</td>
<td>Page 198, Note 4</td>
</tr>
<tr class="odd">
<td>Crate structure</td>
<td>24- AMS- 110.AB.XY</td>
<td>7075-T7351</td>
<td>58.29</td>
<td>28.22</td>
<td>0.48</td>
<td>0.03</td>
<td>Low risk</td>
<td>Note 2</td>
<td>Page 198, Note 4</td>
</tr>
<tr class="even">
<td>XPD board stiffeners</td>
<td>24- AMS- 121.03.XY</td>
<td>6061-T651</td>
<td>39.45</td>
<td>21.77</td>
<td>0.55</td>
<td>0.21</td>
<td>Low risk</td>
<td>Note 2</td>
<td><p>Page 173,</p>
<p>Note 4</p></td>
</tr>
<tr class="odd">
<td>Links</td>
<td>24- AMS- 130.01.XY</td>
<td>7075-T7351</td>
<td>53.58</td>
<td>20.16</td>
<td>0.38</td>
<td>0.33</td>
<td>Low risk</td>
<td>Note 2</td>
<td>Page 198, Note 4</td>
</tr>
<tr class="even">
<td>Top bracket plate</td>
<td>24- AMS- 310.02.XY</td>
<td>7075-T7352</td>
<td>53.58</td>
<td>24.55</td>
<td>0.46</td>
<td>0.09</td>
<td>Low risk</td>
<td>Note 2</td>
<td>Page 196, Note 4</td>
</tr>
<tr class="odd">
<td>Mid bracket bar</td>
<td>24- AMS- 320.02.XY</td>
<td>7075-T7351</td>
<td>53.58</td>
<td>25.47</td>
<td>0.48</td>
<td>0.05</td>
<td>Low risk</td>
<td>Note 2</td>
<td>Page 196, Note 4</td>
</tr>
<tr class="even">
<td>Lower bracket plate</td>
<td>24- AMS- 330-AB.XY</td>
<td>7075-T7351</td>
<td>56.41</td>
<td>9.15</td>
<td>0.16</td>
<td>&gt;2.0</td>
<td>Low risk</td>
<td>Note 2</td>
<td>Page 196, Note 4</td>
</tr>
<tr class="odd">
<td colspan="10"><strong>Fasteners</strong></td>
</tr>
<tr class="even">
<td>Item</td>
<td>Drawing Number</td>
<td>Material and temper</td>
<td>Material allowable stress (ksi)</td>
<td>Max. applied Load (lbf)</td>
<td>Ratio of applied limit stress to allowable stress</td>
<td>Margin of Safety (ult) FS =1.0</td>
<td>Fracture Classification</td>
<td>Rationale</td>
<td>Comments</td>
</tr>
<tr class="odd">
<td>USS to mid Bracket</td>
<td>Joint 1b</td>
<td><p>NAS1351N4</p>
<p>A 286 0.25-28</p></td>
<td>160</td>
<td>Tension = 1156 Shear = 844</td>
<td>0.67</td>
<td>0.04</td>
<td>fail-safe</td>
<td>Note 3</td>
<td><p>Joint Separation,</p>
<p>Page 325, Note 4</p></td>
</tr>
<tr class="even">
<td>Brackets to Electronic boxes/upper</td>
<td>Joint 2a</td>
<td><p>EWB-0420-3</p>
<p>A 286 0.190-32</p></td>
<td>200</td>
<td><p>Tension =494</p>
<p>Shear = 652</p></td>
<td>0.77</td>
<td>0.34</td>
<td>fail-safe</td>
<td>Note 3</td>
<td><p>Combined tension and shear, Page 327,</p>
<p>Note 4</p></td>
</tr>
<tr class="odd">
<td>Main radiator/ Electronic boxes Joints</td>
<td>Joint 3b</td>
<td><p>NAS1351N4</p>
<p>A 286 0.250-28</p></td>
<td>160</td>
<td><p>Tension = 78</p>
<p>Shear = 970</p></td>
<td>0.66</td>
<td>0.71</td>
<td>fail-safe</td>
<td>Note 3</td>
<td><p>Combined tension and shear, Page 330,</p>
<p>Note 4</p></td>
</tr>
<tr class="even">
<td>Links to electronic boxes</td>
<td>Joint 4</td>
<td><p>NAS1351N3</p>
<p>A 286 0.190-32</p></td>
<td>160</td>
<td><p>Tension = 438</p>
<p>Shear = 121</p></td>
<td>0.64</td>
<td>0.26</td>
<td>fail- safe</td>
<td>Note 3</td>
<td><p>Joint Separation,</p>
<p>Page 333, Note 4</p></td>
</tr>
<tr class="odd">
<td>Crates/XPD wall joints</td>
<td>Joint 5a</td>
<td><p>NAS1351N08</p>
<p>A 286 0.164-32</p></td>
<td>160</td>
<td><p>Tension = 151</p>
<p>Shear = 33</p></td>
<td>0.88</td>
<td>0.47</td>
<td>fail-safe</td>
<td>Note 3</td>
<td><p>Combined tension and shear, page 334,</p>
<p>Note 4</p></td>
</tr>
<tr class="even">
<td>TPD wall joints crate</td>
<td>Joint 5b</td>
<td><p>NAS1351N08</p>
<p>A 286 0.164-32</p></td>
<td>160</td>
<td><p>Tension = 227</p>
<p>Shear = 262</p></td>
<td>0.88</td>
<td>0.47</td>
<td>fail-safe</td>
<td>Note 3</td>
<td><p>Combined tension and shear, Page 335,</p>
<p>Note 4</p></td>
</tr>
<tr class="odd">
<td>Upper T Crate wall joints</td>
<td>Joint 5c</td>
<td>A 286 0.190-32 NAS1351N3</td>
<td>160</td>
<td><p>Tension = 894</p>
<p>Shear = 395</p></td>
<td>0.90</td>
<td>0.18</td>
<td>fail-safe</td>
<td>Note 3</td>
<td><p>Joint Separation,</p>
<p>Page 336,</p>
<p>Note 4</p></td>
</tr>
</tbody>
</table>

Notes:

1\) The components will be classified as per JSC25863A, August 1998 to
comply with NASA-STD-5003, October 1996 and SSP 30558 Rev. B, June 1994

2\) The component will be classified as low risk as per section 5.1.L.1,
5.1.L.2.A and 5.1.L.2.B.3 of JSC25863A, and will be shown that the
component possesses acceptable durability(Possesses acceptable
resistance to crack growth)

3\) The component will be classified as fail-safe as per section 5.1.c
of JSC 25863A

4\) Ref. Main Radiators Structural Analysis Report AMS-02-RP-CGS-005,
issue 4, April 5, 2007

**Fracture Classification for High Voltage (HV) Bricks**

  --------------- --------- ------------ ----------- --------- ----------- -------- ---------------- ----------- -----------
  Item            Drawing   Material and Material    Max.      Ratio of    Margin   Fracture         Rationale   Comments
                  Number    temper       allowable   applied   applied     of       Classification               
                                         stress      tensile   limit       Safety                                
                                         (ksi)       stress    stress to   (ult) FS                              
                                                     (ksi)     allowable   =2.0                                  
                                                               stress                                            

  **ECAL and RICH                                                                                                
  HV Bricks**                                                                                                    

  Bracket                   7075-T7351   63.8        14.7      0.23        1.17     Low risk         Note 2      Page 125,
                                                                                                                 Note 4

  Frame                     7075-T7351   59.2        11.8      0.20        1.5      Low risk         Note 2      Page 125,
                                                                                                                 Note 4

  Cover                     6061-T62     39.5        6.8       0.17        1.88     Low risk         Note 2      Page 125,
                                                                                                                 Note 4

  Lateral walls             7075-T7351   63.8        23.8      0.37        0.34     Low risk         Note 2      Page 125,
                                                                                                                 Note 4

  **TOF HV                                                                                                       
  bricks**                                                                                                       

  Frame                     7075-T7351   63.8        11.6      0.18        1.75     Low risk         Note 2      Page 126,
                                                                                                                 Note 4

  Cover                     6061-T62     39.5        14.0      0.35        0.41     Low risk         Note 2      Page126,
                                                                                                                 Note 4

  Vertical Stand            7075-T7351   63.8        11.9      0.19        1.68     Low risk         Note 2      Page 126,
  off                                                                                                            Note 4

  **Fasteners**                                                                                                  

  Item            Drawing   Material and Material    Applied   Ratio of    Margin   Fracture         Rationale   Comments
                  Number    temper       allowable   Load      applied     of       Classification               
                                         stress      (lbf)     limit       Safety                                
                                         (ksi)                 stress to   FS =1.0                               
                                                               allowable                                         
                                                               stress                                            

  **ECAL and RICH                                                                                                
  HV Bricks**                                                                                                    

  HV Bricks to    Joint 1   A 286        160         Tension = 0.73        0.56     fail-safe        Note 3      Combined
  USS                       0.25-28                  444 Shear                                                   tension and
                                                     = 258                                                       shear, Note
                                                                                                                 5

  Lateral wall to Joint 2   A4 70 0.0984 102         Tension = 0.87        0.38     fail-safe        Note 3      Combined
  bracket                   in (2.5 mm)              12 Shear                                                    tension and
                                                     = 107                                                       shear, Note
                                                                                                                 6

  Frame and       Joint 3   A 4 70       102         Tension = 0.87        0.12     fail-safe        Note 3      Combined
  bracket                   0.1181 in (3             271 Shear                                                   tension and
                            mm)                      = 219                                                       shear, Note
                                                                                                                 6

  **TOF HV                                                                                                       
  Bricks**                                                                                                       

  TOF HV bricks   Joint 1   A 286        160         Tension = 0.75        0.25     fail- safe       Note 3      Total
  to Radiators              0.25-28                  141 Shear                                                   thread
                                                     = 134                                                       shear
                                                                                                                 ultimate,
                                                                                                                 Note 5

  Lateral wall to Joint 2   A4 70 0.0984 102         Tension = 0.88        0.68     fail-safe        Note 3      Combined
  Frame                     in (2.5 mm)              38 Shear                                                    tension and
                                                     = 33                                                        shear, Note
                                                                                                                 6

  Vertical stand  Joint 3   A4 70 0.1181 102         Tension = 0.93        0.55     fail-safe        Note 3      Combined
  off to cover              (3 mm)                   153 Shear                                                   tension and
                                                     = 99                                                        shear, Note
                                                                                                                 6
  --------------- --------- ------------ ----------- --------- ----------- -------- ---------------- ----------- -----------

Notes:

1\) The components will be classified as per JSC25863A, August 1998 to
comply with NASA-STD-5003, October 1996 and SSP 30558 Rev. B, June 1994

2\) The component will be classified as low risk as per section 5.1.L.1,
5.1.L.2.A and 5.1.L.2.B.3 of JSC25863A, and will be shown that the
component possesses acceptable durability(Possesses acceptable
resistance to crack growth)

3\) The component will be classified as fail-safe as per section 5.1.c
of JSC 25863A

4\) Ref. HV Bricks Structural analysis Report, AMS-02-RP-CGS-007, issue
1, November. 22, 2004

5\) Ref. AMS-02 Bolt Analysis_Update_v4.(1), 8/4/2005

6\) Ref. AMS-02-DC-CGS-001, issue 1, 8 September 2005

**Fracture Classification of Vacuum Case Components**

<table>
<colgroup>
<col style="width: 11%" />
<col style="width: 9%" />
<col style="width: 10%" />
<col style="width: 7%" />
<col style="width: 9%" />
<col style="width: 10%" />
<col style="width: 8%" />
<col style="width: 9%" />
<col style="width: 7%" />
<col style="width: 14%" />
</colgroup>
<tbody>
<tr class="odd">
<td>Item</td>
<td>Drawing number</td>
<td>Material and temper</td>
<td>Material allowable stress (ksi)</td>
<td>Max. applied tensile stress (ksi)</td>
<td>Ratio of applied limit stress to allowable stress</td>
<td>Margin of Safety (ult) FS=1.4</td>
<td>Fracture Classification</td>
<td>Rationale</td>
<td>Comments</td>
</tr>
<tr class="even">
<td>Outer Cylinder</td>
<td>SDG39135779</td>
<td>7050-T7452 Forging</td>
<td>67</td>
<td>18.9</td>
<td>0.28</td>
<td>1.32</td>
<td>Low risk</td>
<td>Note 2</td>
<td>Sect 3.2.1-14, Note 4</td>
</tr>
<tr class="odd">
<td>Inner Cylinder</td>
<td>SDG39135782</td>
<td>2219-T852 Forging</td>
<td>60</td>
<td>31.4</td>
<td>0.52</td>
<td>0.31</td>
<td>Low risk</td>
<td>Note 2</td>
<td>Sect. 3.3.1-17, Note 4</td>
</tr>
<tr class="even">
<td>Inner cylinder weld</td>
<td>SDG39135782</td>
<td>2219-T852 Forging</td>
<td>32</td>
<td>19.7</td>
<td>0.62</td>
<td>0.116</td>
<td>Fracture critical</td>
<td>Note 5</td>
<td>Sect. 3.3.1-20, Note 4</td>
</tr>
<tr class="odd">
<td>Conical Flanges</td>
<td>SDG39135778</td>
<td>2219-T62 Plate</td>
<td>54</td>
<td>28.7</td>
<td>0.53</td>
<td><p>0.30</p>
<p>0.14 (yield)</p></td>
<td>Low risk</td>
<td>Note 2</td>
<td>Sect.3.3.1-14, Note 4</td>
</tr>
<tr class="even">
<td>Upper Support rings</td>
<td>SDG39135784</td>
<td>7050-T7452 Forging</td>
<td>66</td>
<td>40.85</td>
<td>0.62</td>
<td>0.096</td>
<td>Low risk</td>
<td>Note 2</td>
<td>Sect. 3.4-9, Note 4</td>
</tr>
<tr class="odd">
<td>Lower Support Rings</td>
<td>SEG39135785</td>
<td>7050-T7452 Forging</td>
<td>66</td>
<td>31.47</td>
<td>0.47</td>
<td>0.44</td>
<td>Low risk</td>
<td>Note 2</td>
<td>Sect. 3.5-10, Note 4</td>
</tr>
<tr class="even">
<td>Upper Interface plate Assy</td>
<td>SDG39135788</td>
<td>7050-T7451 plate</td>
<td>68</td>
<td>22.81</td>
<td>0.33</td>
<td>0.96</td>
<td>Low risk</td>
<td>Note 2</td>
<td>Sect. 3.6-5, Note 4</td>
</tr>
<tr class="odd">
<td>Lower Interface plate assy</td>
<td>SDG39135789</td>
<td>7050-T7451 plate</td>
<td>68</td>
<td>13.31</td>
<td>0.19</td>
<td>2.36</td>
<td>Low risk</td>
<td>Note 2</td>
<td>Sect. 3.7-5, Note 4</td>
</tr>
<tr class="even">
<td colspan="10"><strong>Fasteners</strong></td>
</tr>
<tr class="odd">
<td>Item</td>
<td>Drawing Number</td>
<td>Material and temper</td>
<td>Material allowable Load (ksi)</td>
<td>Applied Load (lbf)</td>
<td>Ratio of applied limit stress to allowable stress</td>
<td>Margin of Safety FS =1.0</td>
<td>Fracture Classification</td>
<td>Rationale</td>
<td>Comments</td>
</tr>
<tr class="even">
<td>Upper I/F plate to Vacuum case</td>
<td>SEG39135776</td>
<td><p>NAS1956C</p>
<p>A 286 0.375-24</p></td>
<td>180</td>
<td>Tension = 3942 Shear = 896</td>
<td>0.88</td>
<td>0.176</td>
<td>Fail-safe</td>
<td>Note 3</td>
<td>Joint separation, sect. 3.10.6-19 Note 4</td>
</tr>
<tr class="odd">
<td>Lower Support ring to conical flange</td>
<td>SEG39135776</td>
<td>EWB 0.25-28</td>
<td>200</td>
<td><p>Tension = 724</p>
<p>Shear = 958</p></td>
<td>0.87</td>
<td>0.169</td>
<td>Fail-safe</td>
<td>Note 3</td>
<td>Combined tension and shear ult, sect. 3.10.2-8 Note 4</td>
</tr>
<tr class="even">
<td>Upper Support ring to conical flange</td>
<td>SEG39135776</td>
<td>EWB 0.25-28</td>
<td>200</td>
<td><p>Tension = 716</p>
<p>Shear = 642</p></td>
<td>0.87</td>
<td>0.186</td>
<td>Fail-safe</td>
<td>Note 3</td>
<td>Combined tension and shear ult, sect. 3.10.1-8 Note 4</td>
</tr>
<tr class="odd">
<td>Lower Support ring to outer cylinder</td>
<td>SEG39135776</td>
<td>EWB 0.25-28</td>
<td>200</td>
<td><p>Tension = 824</p>
<p>Shear = 395</p></td>
<td>0.88</td>
<td>0.184</td>
<td>Fail-safe</td>
<td>Note 3</td>
<td><p>Combined tension and shear ult,</p>
<p>sect. 3.10.4 1-9Note 4</p></td>
</tr>
<tr class="even">
<td>Upper Support ring to outer cylinder</td>
<td>SEG39135776</td>
<td>EWB 0.25-28</td>
<td>200</td>
<td><p>Tension =1024</p>
<p>Shear = 391</p></td>
<td>0.87</td>
<td>0.192</td>
<td>Fail-safe</td>
<td>Note 3</td>
<td><p>Combined tension and shear ult,</p>
<p>sect. 3.10.3-9 ,Note 4</p></td>
</tr>
<tr class="odd">
<td>Lower I/F plate to vacuum case</td>
<td>SEG39135776</td>
<td><p>NAS1958C</p>
<p>A 286 ,0.50-20</p></td>
<td>180</td>
<td><p>Tension =2820</p>
<p>Shear = 1805</p></td>
<td>0.86</td>
<td>0.475</td>
<td>Fail-safe</td>
<td>Note 3</td>
<td>Total thread shear ult, sect.3.10.7.2-19, Note 4</td>
</tr>
<tr class="even">
<td>Lower I/F plate to vacuum case</td>
<td>SEG39135776</td>
<td><p>NAS1956C</p>
<p>A 286 ,0.375-24</p></td>
<td>180</td>
<td><p>Tension =1416</p>
<p>Shear = 617</p></td>
<td>0.85</td>
<td>0.505</td>
<td>Fail-safe</td>
<td>Note 3</td>
<td>Combined tension and shear ultimate, sect.3.10.7.1-19, Note 4</td>
</tr>
<tr class="odd">
<td>Clevis plate to upper support ring</td>
<td>SEG39135776</td>
<td>A 286 0.50-20</td>
<td>180</td>
<td>Tension = 6380 Shear = 6387</td>
<td>0.89</td>
<td>0.285</td>
<td>Fail-safe</td>
<td>Note 3</td>
<td>Combined tension and shear ultimate, sect 3.10.5-9, Note 4</td>
</tr>
</tbody>
</table>

Notes:

1\) The components will be classified as per JSC25863A, August 1998 to
comply with NASA-STD-5003, October 1996 and SSP 30558 Rev. B, June 1994.

2\) The component will be classified as low risk as per section 5.1.L.1,
5.1.L.2.A and 5.1.L.2.B.3 of JSC 25863 A and will be shown that the
component possesses acceptable durability (Possesses acceptable
resistance to crack growth)

3\) The component will be classified as fail-safe as per section 5.1.c
of JSC 25863A

4\) Ref.AMS-02 Strength and stability for Vacuum Case analysis report

5\) The component is classified as fracture critical as per sect. 5.2
and will be shown acceptable by compliance with sect. 6.0 of JSC 25863 A

**Fracture Classification of USS Components**

<table>
<colgroup>
<col style="width: 11%" />
<col style="width: 9%" />
<col style="width: 10%" />
<col style="width: 7%" />
<col style="width: 9%" />
<col style="width: 10%" />
<col style="width: 8%" />
<col style="width: 9%" />
<col style="width: 7%" />
<col style="width: 15%" />
</colgroup>
<tbody>
<tr class="odd">
<td>Item</td>
<td>Drawing number</td>
<td>Material and temper</td>
<td>Material allowable stress (ksi)</td>
<td>Max. applied tensile stress (ksi)</td>
<td>Ratio of applied limit stress to allowable stress</td>
<td>Margin of Safety (ult) FS=1.4</td>
<td>Fracture Classification</td>
<td>Rationale</td>
<td>Comments</td>
</tr>
<tr class="even">
<td>Sill Trunnion</td>
<td>SDG39135732</td>
<td>Custom 455 H1000</td>
<td>200</td>
<td>117.5</td>
<td>0.58</td>
<td>0.6(yield)</td>
<td>Fracture critical</td>
<td>Note 2</td>
<td><p>Sect. 2.1.5-42,</p>
<p>Note 5</p></td>
</tr>
<tr class="odd">
<td>Keel Trunnion</td>
<td>SDG39135772</td>
<td>Custom 455 H1000</td>
<td>200</td>
<td>102.7</td>
<td>0.73</td>
<td>0.51 (yield)</td>
<td>Fracture critical</td>
<td>Note 2</td>
<td><p>Sect. 2.3.4-12</p>
<p>Note 5</p></td>
</tr>
<tr class="even">
<td>Upper VC Joint</td>
<td>SDG39135727</td>
<td>7050-T7451 Plate</td>
<td>69</td>
<td>43.8</td>
<td>0.63</td>
<td>0.04</td>
<td>Low risk</td>
<td>Note 3</td>
<td><p>Sect. 2.1.1-10</p>
<p>Note 5</p></td>
</tr>
<tr class="odd">
<td>Lower VC Joint</td>
<td>SDG39135737</td>
<td>7050-T7451 Plate</td>
<td>67</td>
<td>40.7</td>
<td>0.61</td>
<td>0.06</td>
<td>Low risk</td>
<td>Note 3</td>
<td><p>Sect. 2.1.9-13,</p>
<p>Note 5</p></td>
</tr>
<tr class="even">
<td>Sill joint primary secondary</td>
<td>SDG39135730</td>
<td>7050-T7451 Plate</td>
<td>66</td>
<td>26.7</td>
<td>0.40</td>
<td>0.55</td>
<td>Low risk</td>
<td>Note 3</td>
<td>Sect. 2.1.3-10, Note 5</td>
</tr>
<tr class="odd">
<td>Diagonal strut end fitting</td>
<td>SEG39135743</td>
<td>7075-T73511</td>
<td>37</td>
<td>16..2</td>
<td>0.43</td>
<td>0.58</td>
<td>Low risk</td>
<td>Note 3</td>
<td>Sect. 2.1.13.2-5,Note 5</td>
</tr>
<tr class="even">
<td>Lower center body box joint</td>
<td>SDG39135759 SDG39135760</td>
<td>7050-T7451 Plate</td>
<td>70</td>
<td>38.8</td>
<td>0.55</td>
<td>0.18</td>
<td>Low risk</td>
<td>Note 3</td>
<td><p>Sect. 2.2.1-14,</p>
<p>Note 5</p></td>
</tr>
<tr class="odd">
<td>Sill elbow joint</td>
<td>SDG39135734</td>
<td>7050-T7451 Plate</td>
<td>66</td>
<td>35.7</td>
<td>0.54</td>
<td>0.21</td>
<td>Low risk</td>
<td>Note 3</td>
<td>Sect. 2.1.7-22, Note 5</td>
</tr>
<tr class="even">
<td>Keel block</td>
<td>SEG39135770</td>
<td>7050-T7451 Plate</td>
<td>67</td>
<td>26.7</td>
<td>0.40</td>
<td>0.63</td>
<td>Fracture critical</td>
<td>Note 2</td>
<td><p>Sect. 2.3.2-13,</p>
<p>Note 5</p></td>
</tr>
<tr class="odd">
<td>Diagonal sill bracket</td>
<td>SEG39135740</td>
<td>7050-T7451 Plate</td>
<td>66</td>
<td>42.0</td>
<td>0.63</td>
<td>0.03</td>
<td>Fracture critical</td>
<td>Note 2</td>
<td><p>Sect. 2.1.12-2,</p>
<p>Note 5</p></td>
</tr>
<tr class="even">
<td>Sill bracket</td>
<td>SEG39135738</td>
<td>7050-T7451 Plate</td>
<td>66</td>
<td>31.0</td>
<td>0.47</td>
<td>0.40</td>
<td>Low risk</td>
<td>Note 3</td>
<td><p>Sect. 2.1.10-8,</p>
<p>Note 5</p></td>
</tr>
<tr class="odd">
<td>Lower USS to Upper USS joint</td>
<td>SDG39135762</td>
<td>7050-T7451 Plate</td>
<td>66</td>
<td>20.9</td>
<td>0.31</td>
<td>1.15</td>
<td>Low risk</td>
<td>Note 3</td>
<td><p>Sect. 2.2.4-16,</p>
<p>Note 5</p></td>
</tr>
<tr class="even">
<td colspan="10"><strong>Fasteners</strong></td>
</tr>
<tr class="odd">
<td>Item</td>
<td>Drawing Number</td>
<td>Material and temper</td>
<td>Material allowable stress (ksi)</td>
<td>Applied Load (lbf)</td>
<td>Ratio of applied limit stress to allowable stress</td>
<td>Margin of Safety FS =1.0</td>
<td>Fracture Classification</td>
<td>Rationale</td>
<td>Comments</td>
</tr>
<tr class="even">
<td>Upper I/F plate to USS-02</td>
<td>SDG39135726</td>
<td><p>NAS1958C</p>
<p>A 286 0.50-20</p></td>
<td>180</td>
<td>Tension = 4037 Shear = 811</td>
<td>0.91</td>
<td>0.404</td>
<td>Fail-safe</td>
<td>Note 4</td>
<td>Combined tension and shear ultimate, sect. 2.4.1.1-19, Note 5</td>
</tr>
<tr class="odd">
<td>Lower I/F plate to USS-02</td>
<td>SEG39135726</td>
<td><p>NAS1958C</p>
<p>A 286 0.50-20</p></td>
<td>180</td>
<td>Tension = 3008 Shear = 1973</td>
<td>0.90</td>
<td>0.418</td>
<td>Fail-safe</td>
<td>Note 4</td>
<td>Combined tension and shear ultimate, Sect.2.4.1.2-19, Note 5</td>
</tr>
<tr class="even">
<td>Sill bracket to sill joint</td>
<td>SEG39135726</td>
<td><p>NAS1958C</p>
<p>A 286 0.50-20</p></td>
<td>180</td>
<td><p>Tension=5627</p>
<p>Shear =68</p></td>
<td>0.91</td>
<td>0.444</td>
<td>Fail-safe</td>
<td>Note 4</td>
<td>Combined tension and shear ultimate, Sect.2.4.1.4-17, Note 5</td>
</tr>
<tr class="odd">
<td>Lower USS to Upper USS bolts</td>
<td>SEG39135724</td>
<td><p>NAS1958C</p>
<p>A 286 0.50-20</p></td>
<td>180</td>
<td><p>Tension = 6342</p>
<p>Shear = 3953</p></td>
<td>0.91</td>
<td>0.050</td>
<td>Fail-safe</td>
<td>Note 4</td>
<td>Joint separation, Sect.2.4.2.1-19,Note 5</td>
</tr>
<tr class="even">
<td>Lower angle beam to centerbody box joint</td>
<td>SEG39135758</td>
<td><p>EWB0420</p>
<p>0.50-20</p></td>
<td>200</td>
<td>Tension = 7663 Shear =587</td>
<td>0.88</td>
<td>0.088</td>
<td>Fail-safe</td>
<td>Note 4</td>
<td>Total thread shear ultimate, Sect.2.4.2.2-17, Note 5</td>
</tr>
<tr class="odd">
<td>Diagonal sill bracket to sill joint</td>
<td>SEG39135726</td>
<td><p>EWB0420</p>
<p>0.50-20</p></td>
<td>200</td>
<td>Tension = 14894 Shear = 2192</td>
<td>0.94</td>
<td>0.115</td>
<td>Fail-safe</td>
<td>Note 4</td>
<td>Combined tension and shear ultimate, sect. 2.4.1.5-18. Negative M.S.
on joint separation is acceptable for fail-safe cases</td>
</tr>
<tr class="even">
<td>Keel angle joint to lower USS-02 assy bolts</td>
<td>SEG39135724</td>
<td><p>EWB0420</p>
<p>0.50-20</p></td>
<td>200</td>
<td>Tension = 2766 Shear = 1491</td>
<td>0.85</td>
<td>0.067</td>
<td>Fail-safe</td>
<td>Note 4</td>
<td>Total thread shear ultimate, Sect. 2.4.3.1-17, Note 5</td>
</tr>
<tr class="odd">
<td>Keel retainer to keel trunnion and keel block</td>
<td>SEG39135768</td>
<td><p>NAS8103,</p>
<p>0.190-32</p></td>
<td>160</td>
<td>Tension = 374 Shear = 0</td>
<td>0.86</td>
<td>0.435</td>
<td>Fail-safe</td>
<td>Note 4</td>
<td>Total tension ult., Sect. 2.4.3.2-8, Note 5</td>
</tr>
<tr class="even">
<td>Vertex bracket to PAS platform</td>
<td>SEG39135812</td>
<td>A 286 0.375-24</td>
<td>180</td>
<td><p>Tension =319</p>
<p>Shear =774</p></td>
<td>0.69</td>
<td>0.37</td>
<td>Fail-safe</td>
<td>Note 4</td>
<td>Combined tension and shear ultimate, Note 5</td>
</tr>
<tr class="odd">
<td>Rear bracket to PAS platform</td>
<td>SEG39135812</td>
<td><p>EWB 0420</p>
<p>0.375-24</p></td>
<td>200</td>
<td>Tension = 2507 Shear =6351</td>
<td>0.79</td>
<td>0.019</td>
<td>Fail-safe</td>
<td>Note 4</td>
<td>Combined tension and shear ultimate, Note 5</td>
</tr>
</tbody>
</table>

Notes:

1\) The components will be classified as per JSC25863A, August 1998 to
comply with NASA-STD-5003, October 1996 and SSP 30558 Rev. B, June 1994.

2\) The component will be classified as fracture critical as per sect
5.2 and will be shown acceptable by compliance with sect. 6.0 of
JSC25863A

3\) The component will be classified as low risk as per section 5.1.L.1,
5.1.L.2.A and 5.1.L.2.B.3 of JSC 25863A and will be shown that the
component possesses acceptable durability (Possesses acceptable
resistance to crack growth)

4\) The component will be classified as fail-safe as per section 5.1.c
of JSC 25863 A

5\) Ref. AMS-02, Strength and Stability for USS-02 Stress analysis
Report

**Fracture Classification of AMS-02 PAS**

<table>
<colgroup>
<col style="width: 11%" />
<col style="width: 9%" />
<col style="width: 10%" />
<col style="width: 7%" />
<col style="width: 9%" />
<col style="width: 10%" />
<col style="width: 8%" />
<col style="width: 9%" />
<col style="width: 7%" />
<col style="width: 15%" />
</colgroup>
<tbody>
<tr class="odd">
<td>Item</td>
<td>Drawing number</td>
<td>Material and temper</td>
<td>Material allowable stress (ksi)</td>
<td>Max. applied tensile stress (ksi)</td>
<td>Ratio of applied limit stress to allowable stress</td>
<td>Margin of Safety (ult) FS=1.4</td>
<td>Fracture Classification</td>
<td>Rationale</td>
<td>Comments</td>
</tr>
<tr class="even">
<td>PAS platform</td>
<td>SDG39135817</td>
<td>7050 T7451 plate</td>
<td>73</td>
<td>31.339</td>
<td>0.43</td>
<td>0.072</td>
<td>Low risk</td>
<td>Note 2</td>
<td><p>Sect. 4.3-6,</p>
<p>Note 5</p></td>
</tr>
<tr class="odd">
<td>Capture bar</td>
<td>SDG39135849</td>
<td>A 286 bar</td>
<td>130</td>
<td>59.321</td>
<td>0.45</td>
<td>0.052</td>
<td>Low risk</td>
<td>Note 2</td>
<td><p>Sect. 4.11.1-7</p>
<p>Note 5</p></td>
</tr>
<tr class="even">
<td>Bridge beam</td>
<td>SDG39135838</td>
<td>7050-T7451 Plate</td>
<td>73</td>
<td>31.047</td>
<td>0.43</td>
<td>0.082</td>
<td>Low risk</td>
<td>Note 2</td>
<td><p>Sect.4.6-9</p>
<p>Note 5</p></td>
</tr>
<tr class="odd">
<td>Bearing housing</td>
<td>SDG39135845</td>
<td>15-5PH H1025</td>
<td>155</td>
<td>123.58</td>
<td>0.79</td>
<td>0.236</td>
<td>Low risk</td>
<td>Note 2</td>
<td>Sect. 4.10-8</td>
</tr>
</tbody>
</table>

Notes:

1\) The components will be classified as per JSC25863A, August 1998 to
comply with NASA-STD-5003, October 1996 and SSP 30558 Rev. B, June 1994.

2\) The component will be classified as fracture critical as per sect
5.2 and will be shown acceptable by compliance with sect. 6.0 of
JSC25863A

3\) The component will be classified as low risk as per section 5.1.L.1,
5.1.L.2.A and 5.1.L.2.B.3 of JSC 25863A and will be shown that the
component possesses acceptable durability (Possesses acceptable
resistance to crack growth)

4\) The component will be classified as fail-safe as per section 5.1.c
of JSC 25863 A

5\) Ref. AMS-02, Strength and Stability for USS-02 Stress analysis
Report

6\) Ref. AMS-02 PAS analysis report

**Fracture Classification of AMS-02 UPS**

<table>
<colgroup>
<col style="width: 11%" />
<col style="width: 9%" />
<col style="width: 10%" />
<col style="width: 7%" />
<col style="width: 9%" />
<col style="width: 10%" />
<col style="width: 8%" />
<col style="width: 9%" />
<col style="width: 7%" />
<col style="width: 14%" />
</colgroup>
<tbody>
<tr class="odd">
<td>Item</td>
<td>Drawing number</td>
<td>Material and temper</td>
<td>Material allowable stress (ksi)</td>
<td>Max. applied stress (ksi)</td>
<td>Ratio of applied stress to allowable stress</td>
<td>Margin of Safety (ult) FS=2.0</td>
<td>Fracture Classification</td>
<td>Rationale</td>
<td>Comments</td>
</tr>
<tr class="even">
<td>UPS boxes</td>
<td></td>
<td>7075-T7351</td>
<td>66</td>
<td>5.39</td>
<td>0.08</td>
<td>5.13</td>
<td>Low risk</td>
<td>Note 2</td>
<td>Note 3, page 6</td>
</tr>
<tr class="odd">
<td colspan="10"><strong>Fasteners</strong></td>
</tr>
<tr class="even">
<td>Item</td>
<td>Drawing Number</td>
<td>Material and temper</td>
<td>Material allowable stress (ksi)</td>
<td>Applied Load (lbf)</td>
<td>Ratio of applied limit stress to allowable stress</td>
<td>Margin of Safety FS =1.0</td>
<td>Fracture Classification</td>
<td>Rationale</td>
<td>Comments</td>
</tr>
<tr class="odd">
<td>UPS Box to bracket bolts</td>
<td></td>
<td>NAS1351N4, 0.25-28 A-286</td>
<td>160</td>
<td><p>Tension = 159</p>
<p>Shear = 395</p></td>
<td>0.74</td>
<td>0.27</td>
<td>Fail-safe</td>
<td>Note 4</td>
<td><p>Total thread shear,</p>
<p>Note 5, page 10</p></td>
</tr>
<tr class="even">
<td>Bracket to USS bolts</td>
<td></td>
<td><p>NAS1954,</p>
<p>0.25-28 A-286</p></td>
<td>180</td>
<td><p>Tension = 178</p>
<p>Shear = 204</p></td>
<td>0.75</td>
<td>0.82</td>
<td>Fail-safe</td>
<td>Note 4</td>
<td>Combined tension and shear, Note 4, page 10</td>
</tr>
</tbody>
</table>

Notes:

1\) The components will be classified as per JSC25863A, August 1998 to
comply with NASA-STD-5003, October 1996 and SSP 30558 Rev. B, June 1994.

2\) The component will be classified as low risk as per sect. 5.1.L.1,
5.1.L.2. A, 5.1.L.2.B3 of JSC25863 A and will be shown that the
component possesses acceptable durability (possesses acceptable
resistance to crack growth)

3\) Ref. UPS Box Redesign Structural Analysis report, CSIST, Taiwan,
December 28, 2005

4\) The component will be classified as fail-safe based on sect. 5.1 c
of JSC 25863 A

5\) Ref. UPS Box Redesign Structural analysis report, 12 December 2005

Fracture Classification of AMS-02 E-Crates

<table>
<colgroup>
<col style="width: 11%" />
<col style="width: 9%" />
<col style="width: 10%" />
<col style="width: 7%" />
<col style="width: 9%" />
<col style="width: 10%" />
<col style="width: 8%" />
<col style="width: 9%" />
<col style="width: 7%" />
<col style="width: 14%" />
</colgroup>
<tbody>
<tr class="odd">
<td>Item</td>
<td>Drawing number</td>
<td>Material and temper</td>
<td>Material allowable stress (ksi)</td>
<td>Max. applied tensile stress (ksi)</td>
<td>Ratio of applied limit stress to allowable stress</td>
<td>Margin of Safety (ult) FS=2.0</td>
<td>Fracture Classification</td>
<td>Rationale</td>
<td>Comments</td>
</tr>
<tr class="even">
<td>Bottom plate</td>
<td></td>
<td>7075-T7351</td>
<td>62.9</td>
<td>13.5</td>
<td>0.21</td>
<td>1.34</td>
<td>Low risk</td>
<td>Note 2</td>
<td>Page 50, Note 5</td>
</tr>
<tr class="odd">
<td>Lateral wall</td>
<td></td>
<td>7075-T7351</td>
<td>62.9</td>
<td>8.9</td>
<td>0.14</td>
<td>2.53</td>
<td>Low risk</td>
<td>Note 2</td>
<td>Page 50, Note 5</td>
</tr>
<tr class="even">
<td colspan="10"><strong>Fasteners</strong></td>
</tr>
<tr class="odd">
<td>Item</td>
<td>Drawing Number</td>
<td>Material and temper</td>
<td>Material allowable stress (ksi)</td>
<td>Applied Load (lbf)</td>
<td>Ratio of applied limit stress to allowable stress</td>
<td>Margin of Safety FS =1.0</td>
<td>Fracture Classification</td>
<td>Rationale</td>
<td>Comments</td>
</tr>
<tr class="even">
<td>E-Crates to USS-02</td>
<td>Joint 1</td>
<td>A 286 0.190-32 NAS1351N3</td>
<td>160</td>
<td><p>Tension = 1202</p>
<p>Shear = 248</p></td>
<td>0.85</td>
<td>0.22</td>
<td>Fail-safe</td>
<td>Note 3</td>
<td>Total thread shear ultimate, Note 4</td>
</tr>
<tr class="odd">
<td>Lateral walls to bottom plate</td>
<td>Joint 2</td>
<td>A 286 0.190-32 NAS1351N3</td>
<td>160</td>
<td><p>Tension = 545</p>
<p>Shear = 679</p></td>
<td>0.81</td>
<td>0.28</td>
<td>Fail-safe</td>
<td>Note 3</td>
<td>Combined tension and shear, Note 4</td>
</tr>
<tr class="even">
<td>Side wall bolts</td>
<td>Joint 3</td>
<td>A 286 0.164-32 NAS1351N08</td>
<td>160</td>
<td><p>Tension = 391</p>
<p>Shear = 315</p></td>
<td>0.81</td>
<td>0.39</td>
<td>Fail-safe</td>
<td>Note 3</td>
<td>Combined tension and shear, Note 4</td>
</tr>
</tbody>
</table>

Notes:

1\) The components will be classified as per JSC25863A, August 1998 to
comply with NASA-STD-5003, October 1996 and SSP 30558 Rev. B, June 1994.

2\) The component will be classified as low risk as per section 5.1.L.1,
5.1.L.2.A and 5.1.L.2.B.3 of JSC 25863 A and will be shown that the
component possesses acceptable durability (Possesses acceptable
resistance to crack growth)

3\) The component will be classified as fail-safe as per section 5.1.c
of JSC 25863A

4\) Ref. AMS-02 Bolt Analysis_Update_v4.(1), 8/4/2005

5\) Ref. AMS02-RP-CGS-003, issue 2, 4 August, 2005, Carlo Gavazzi Space

Fracture Classification of AMS-02 Cryomagnet Avionics Box (CAB)

<table style="width:100%;">
<colgroup>
<col style="width: 8%" />
<col style="width: 12%" />
<col style="width: 9%" />
<col style="width: 8%" />
<col style="width: 10%" />
<col style="width: 10%" />
<col style="width: 10%" />
<col style="width: 9%" />
<col style="width: 6%" />
<col style="width: 12%" />
</colgroup>
<tbody>
<tr class="odd">
<td>Item</td>
<td><p>Drawing</p>
<p>number</p></td>
<td><p>Material and</p>
<p>temper</p></td>
<td><p>Material</p>
<p>Allowable</p>
<p>stress (ksi)</p></td>
<td><p>Max. applied</p>
<p>tensile</p>
<p>stress (ksi)</p></td>
<td><p>Ratio of applied</p>
<p>limit stress to</p>
<p>allowable stress</p></td>
<td><p>Margin of</p>
<p>Safety (ult)</p>
<p>FS=2.0</p></td>
<td><p>Fracture</p>
<p>Classification</p></td>
<td>Rationale</td>
<td>Comments</td>
</tr>
<tr class="even">
<td>Base plate</td>
<td><p>AMS-AD-</p>
<p>CAB-00000-CRS</p></td>
<td>6061-T6</td>
<td>42.0</td>
<td>3.79</td>
<td>0.21</td>
<td>5.0</td>
<td>Low risk</td>
<td>Note 2</td>
<td>Page 34, Note 5</td>
</tr>
<tr class="odd">
<td colspan="10"><strong>Fasteners</strong></td>
</tr>
<tr class="even">
<td>Item</td>
<td>Drawing Number</td>
<td>Material and temper</td>
<td>Material allowable stress (ksi)</td>
<td>Applied Load (lbf)</td>
<td>Ratio of applied limit stress to allowable stress</td>
<td>Margin of Safety FS =1.0</td>
<td>Fracture Classification</td>
<td>Rationale</td>
<td>Comments</td>
</tr>
<tr class="odd">
<td>CAB to USS bolts</td>
<td><p>AMS-AD-</p>
<p>CAB-00000-CRS</p></td>
<td>A 286 0.25-28 NAS1954C</td>
<td>180</td>
<td></td>
<td></td>
<td></td>
<td>Fail-safe</td>
<td>Note 4</td>
<td>There are 32 bolts attaching the CAB to USS. Fail-safe by
Engineering Judgment</td>
</tr>
<tr class="even">
<td>CAB internal screws</td>
<td><p>AMS-AD-</p>
<p>CAB-00000-CRS</p></td>
<td>AISI 304, M4, M3, and M2.5 screws</td>
<td>101.5</td>
<td></td>
<td></td>
<td></td>
<td>Fail-safe</td>
<td>Note 4</td>
<td>There are multiple screws. Fail-safe by Engineering Judgment</td>
</tr>
</tbody>
</table>

Notes:

1\) The components will be classified as per JSC25863A, August 1998 to
comply with NASA-STD-5003, October 1996 and SSP 30558 Rev. B, June 1994.

2\) The component will be classified as low risk as per section 5.1.L.1,
5.1.L.2.A and 5.1.L.2.B.3 of JSC 25863 A and will be shown that the
component possesses acceptable durability (Possesses acceptable
resistance to crack growth)

3\) The component will be classified as fail-safe as per section 5.1.c
of JSC 25863A

4\) The component is classified as fail-safe by Engineering judgment as
per section 5.1.c of JSC 25863A

5\) Ref. AMS-02 Cryomagnet Avionics Box, Mechanical Analysis,
CAB-AN-CRS-0055, issue 2, September 22, 2006, EADS Astrium CRISA

+--------+--------+--------+----------+------+------+-------+-------+
| **Fr   |        |        |          |      |      |       |       |
| acture |        |        |          |      |      |       |       |
| C      |        |        |          |      |      |       |       |
| ertifi |        |        |          |      |      |       |       |
| cation |        |        |          |      |      |       |       |
| for    |        |        |          |      |      |       |       |
| TRD    |        |        |          |      |      |       |       |
| Com    |        |        |          |      |      |       |       |
| posite |        |        |          |      |      |       |       |
| Struct |        |        |          |      |      |       |       |
| ures** |        |        |          |      |      |       |       |
+--------+--------+--------+----------+------+------+-------+-------+
| **     | *      | **Man  | **Basis  | **Q  | **N  | **S   | **D   |
| Compon | *Mater | ufactu | for      | uali | DE** | ample | amage |
| ents** | ials** | rers** | ma       | ty** |      | te    | cont  |
|        |        |        | terial** |      | **   | sts** | rol** |
|        |        | **     |          | **C  | Tech |       |       |
|        |        | Name** | **prop   | ontr | niqu |       |       |
|        |        |        | erties** | ol** | es** |       |       |
+--------+--------+--------+----------+------+------+-------+-------+
| O      | Carbon | ADCO   | ADCO     | Note | Note | Notes | Note  |
| ctagon | fiber  | Gmbh   |          | 8    | 2,   | 1     | 10    |
| Panels | skin   |        | Data     |      | 9a   | ,3,4, |       |
|        |        | Aachen | sheets   |      |      | 5,6,7 |       |
| sid    | M4     |        |          |      |      |       |       |
| ewalls | 0JB/EP | G      |          |      |      |       |       |
|        |        | ernany |          |      |      |       |       |
|        | Honey  |        |          |      |      |       |       |
|        | comb   |        |          |      |      |       |       |
|        |        |        |          |      |      |       |       |
|        | Al.    |        |          |      |      |       |       |
|        | 5056   |        |          |      |      |       |       |
|        | core   |        |          |      |      |       |       |
+--------+--------+--------+----------+------+------+-------+-------+
| Bul    | Carbon | ADCO   | ADCO     | Note | Note |       | Note  |
| kheads | fiber  | Gmbh   |          | 8    | 9b   |       | 10    |
|        | skin   |        | Data     |      |      |       |       |
|        |        | Aachen | sheets   |      |      |       |       |
|        | M4     |        |          |      |      |       |       |
|        | 0JB/EP | G      |          |      |      |       |       |
|        |        | ermany |          |      |      |       |       |
|        | Honey  |        |          |      |      |       |       |
|        | comb   |        |          |      |      |       |       |
|        |        |        |          |      |      |       |       |
|        | Al.    |        |          |      |      |       |       |
|        | 5056   |        |          |      |      |       |       |
|        | core   |        |          |      |      |       |       |
+--------+--------+--------+----------+------+------+-------+-------+
| Upper  | Carbon | ADCO   | ADCO     | Note | Note |       | Note  |
| plate  | fiber  | Gmbh   |          | 8    | 2,   |       | 10    |
|        | skin   |        | Data     |      | 9b   |       |       |
|        |        | Aachen | sheets   |      |      |       |       |
|        | M4     |        |          |      |      |       |       |
|        | 0JB/EP | G      |          |      |      |       |       |
|        |        | ermany |          |      |      |       |       |
|        | Honey  |        |          |      |      |       |       |
|        | comb   |        |          |      |      |       |       |
|        |        |        |          |      |      |       |       |
|        | Al.    |        |          |      |      |       |       |
|        | 5056   |        |          |      |      |       |       |
|        | core   |        |          |      |      |       |       |
+--------+--------+--------+----------+------+------+-------+-------+
| Lower  | Carbon | Euro   | Euro     | Note | Note |       | Note  |
| cover  | fiber  | comp   | Co       | 8    | 2,   |       | 10    |
|        | skin   | osites | mposites |      | 9b   |       |       |
|        |        |        |          |      |      |       |       |
|        | T      | Echt   | Data     |      |      |       |       |
|        | 300/EP | ernach | sheets   |      |      |       |       |
|        |        |        |          |      |      |       |       |
|        | Honey  | Luxe   |          |      |      |       |       |
|        | comb   | mbourg |          |      |      |       |       |
|        |        |        |          |      |      |       |       |
|        | Al.    |        |          |      |      |       |       |
|        | 5056   |        |          |      |      |       |       |
|        | core   |        |          |      |      |       |       |
+--------+--------+--------+----------+------+------+-------+-------+
| R      | Carbon | Euro   | Euro     | Note | Note |       | Note  |
| einfor | fibre  | comp   | Co       | 8    | 9b   |       | 10    |
| cement | T      | osites | mposites |      |      |       |       |
| Rings  | 300/EP |        |          |      |      |       |       |
|        |        | Echt   | Data     |      |      |       |       |
|        |        | ernach | sheets   |      |      |       |       |
|        |        |        |          |      |      |       |       |
|        |        | Luxe   |          |      |      |       |       |
|        |        | mbourg |          |      |      |       |       |
+--------+--------+--------+----------+------+------+-------+-------+

Notes:

1\) TRD Octagon panels Pull Test, RWTH, Aachen, 3/15/2005

2\) Venting of parts of TRD detector, RWTH, Aachen,12/13/2004

3\) Side Panel skin tension and Bending test samples, ams 2000a

4\) Side panel bending test coupons, ams2001a

5\) Side Panel Joint test coupon, ams2003_1a

6\) Side Panel Corner Junction test coupon, ams2003_2a

7\) Panel specimen locations, ams2004a

8\) Manufacturer Certificate of Conformance is supplied

9a) NDE includes visual inspection and dimensional verification on 3D
measuring device as well as static load test(including acoustic loads)
on a sample side panel( RWTH, Aachen/ISAtec, 19/1/2004)

9b) NDE includes visual inspection and dimensional verification on 3D
measuring device

10\) Damage control will be implemented by careful handling and
inspection to assure quality of the hardware

+-----------+-------+---------+-------+-----+-------+-------+--------+
| *         |       |         |       |     |       |       |        |
| *Fracture |       |         |       |     |       |       |        |
| Cert      |       |         |       |     |       |       |        |
| ification |       |         |       |     |       |       |        |
| for TRD   |       |         |       |     |       |       |        |
| Gas       |       |         |       |     |       |       |        |
| System    |       |         |       |     |       |       |        |
| Composite |       |         |       |     |       |       |        |
| Str       |       |         |       |     |       |       |        |
| uctures** |       |         |       |     |       |       |        |
+-----------+-------+---------+-------+-----+-------+-------+--------+
| **Com     | **    | **M     | **    | **  | **    | **S   | **Da   |
| ponents** | Mater | anufact | Basis | Qua | NDE** | ample | mage** |
|           | ial** | urers** | for   | lit |       | te    |        |
|           |       |         | mater | y** | **Te  | sts** | **C    |
|           |       | *       | ial** |     | chniq |       | ontrol |
|           |       | *Name** |       | **  | ues** |       | Plan** |
|           |       |         | **pr  | Con |       |       |        |
|           |       |         | opert | tro |       |       |        |
|           |       |         | ies** | l** |       |       |        |
+-----------+-------+---------+-------+-----+-------+-------+--------+
| Xenon     | C     | ARDE    | ARDE  | N   | Note  | Note1 | Note   |
| tank      | arbon |         |       | ote | 5     |       | 10     |
|           | fiber |         | Ca    | 4   |       |       |        |
|           |       |         | talog |     |       |       |        |
|           | o     |         |       |     |       |       |        |
|           | verwr |         |       |     |       |       |        |
|           | apped |         |       |     |       |       |        |
|           |       |         |       |     |       |       |        |
|           | stai  |         |       |     |       |       |        |
|           | nless |         |       |     |       |       |        |
|           | steel |         |       |     |       |       |        |
+-----------+-------+---------+-------+-----+-------+-------+--------+
| CO2 tank  | C     | ARDE    | ARDE  | N   | Note  | Note  | Note   |
|           | arbon |         |       | ote | 5     | 2     | 10     |
|           | fiber |         | Ca    | 4   |       |       |        |
|           |       |         | talog |     |       |       |        |
|           | o     |         |       |     |       |       |        |
|           | verwr |         |       |     |       |       |        |
|           | apped |         |       |     |       |       |        |
|           |       |         |       |     |       |       |        |
|           | stai  |         |       |     |       |       |        |
|           | nless |         |       |     |       |       |        |
|           | steel |         |       |     |       |       |        |
+-----------+-------+---------+-------+-----+-------+-------+--------+
| Straw     | K     | Lamina  | Ma    | N   | Note  | Note  | Note   |
| tubes     | apton | die     | nufac | ote | 6     | 9     | 10     |
|           |       | lectics | turer | 4   |       |       |        |
|           |       |         |       | a,8 |       |       |        |
|           |       | West    | Ca    |     |       |       |        |
|           |       | Sussex, | talog |     |       |       |        |
|           |       | UK      |       |     |       |       |        |
+-----------+-------+---------+-------+-----+-------+-------+--------+
| Lon       | C     | Secar   | Ma    | N   | Note  | Note  | Note   |
| gitudinal | arbon |         | nufac | ote | 7     | 9     | 10     |
| s         | fiber | Murzzu  | turer | 4   |       |       |        |
| tiffeners |       | sschlag |       | a,8 |       |       |        |
|           |       |         | Ca    |     |       |       |        |
|           |       | Austria | talog |     |       |       |        |
+-----------+-------+---------+-------+-----+-------+-------+--------+
| T         | C     | Secar   | Ma    | N   | Note  | Note  | Note   |
| ransverse | arbon |         | nufac | ote | 7     | 9     | 10     |
| s         | fiber | Murzzu  | turer | 4   |       |       |        |
| tiffeners |       | sschlag |       | a,8 |       |       |        |
|           |       |         | Ca    |     |       |       |        |
|           |       | Austria | talog |     |       |       |        |
+-----------+-------+---------+-------+-----+-------+-------+--------+

Notes:

1\) ARDE Qualification by similarity Report of Xenon Tank PN D4815 to PN
D 4636, EG10330, July 6, 2001

2\) ARDE Qualification by similarity Report of CO2 Tank PN D4816 to PN
D4683, EG10331 July 6, 2001

3\) NDE tests on straw tubes by pressure drop measurement at 1.8 bar
overpressure

4\) Manufacturers Certificate of Compliance will be supplied

4a) Manufacturers Certificate of compliance is supplied

5\) ARDE tanks are ultrasonically inspected

6\) NDE on Straw tubes is done by pressure drop measurement at 1.8 bar
overpressure

7\) NDE on Longitudinal and transverse stiffeners include visual
inspection, Dimensional and straightness verification

8\) Assembly work of straw tubes, Longitudinal and transverse stiffeners
are done at the clean room in Aachen, Germany

9\) Sample tests include determination of Modulus of elasticity by Eigen
frequency on a shaker

10\) Damage Control plan will be implemented as per ANSI/AIAA-S081

+----------+-------+---------+--------+-----+--------+------+-------+
| **       |       |         |        |     |        |      |       |
| Fracture |       |         |        |     |        |      |       |
| Certi    |       |         |        |     |        |      |       |
| fication |       |         |        |     |        |      |       |
| for      |       |         |        |     |        |      |       |
| Silicon  |       |         |        |     |        |      |       |
| Tracker  |       |         |        |     |        |      |       |
| C        |       |         |        |     |        |      |       |
| omposite |       |         |        |     |        |      |       |
| Stru     |       |         |        |     |        |      |       |
| ctures** |       |         |        |     |        |      |       |
+----------+-------+---------+--------+-----+--------+------+-------+
| **Com    | **    | **M     | *      | **  | *      | **Sa | **D   |
| ponent** | Mater | anufact | *Basis | Qua | *NDE** | mple | amage |
|          | ial** | urers** | for    | lit |        | tes  | Co    |
|          |       |         | mate   | y** | **     | ts** | ntrol |
|          |       | *       | rial** |     | Techni |      | p     |
|          |       | *Name** |        | **  | ques** |      | lan** |
|          |       |         | **     | Con |        |      |       |
|          |       |         | proper | tro |        |      |       |
|          |       |         | ties** | l** |        |      |       |
+----------+-------+---------+--------+-----+--------+------+-------+
| Tracker  | C     | Co      | Con    | N   | Note 4 | N    | Note  |
| planes   | arbon | ntraves | traves | ote |        | otes | 5     |
| Sandwich | fiber | AG      |        | 1   |        | 2    |       |
| facing   |       |         | C      |     |        |      |       |
|          | HYE   | Zurich  | atalog |     |        |      |       |
|          | 34    |         |        |     |        |      |       |
|          | 54-3J |         |        |     |        |      |       |
|          |       |         |        |     |        |      |       |
|          | M55   |         |        |     |        |      |       |
|          | To    |         |        |     |        |      |       |
|          | rayca |         |        |     |        |      |       |
|          |       |         |        |     |        |      |       |
|          | Fib   |         |        |     |        |      |       |
|          | erite |         |        |     |        |      |       |
+----------+-------+---------+--------+-----+--------+------+-------+
| Tracker  | Al.   | Hexcel  | Hexcel | N   | Note 4 | Note | Note  |
| planes   | core  |         |        | ote |        | 3    | 5     |
| Sandwich | 5056  |         | C      | 1   |        |      |       |
| core     |       |         | atalog |     |        |      |       |
+----------+-------+---------+--------+-----+--------+------+-------+
| Tracker  | C     | ADCO,   | ADCO   | N   | Note 4 | None | Note  |
| Shell    | arbon | Aachen  |        | ote |        |      | 5     |
|          | fiber |         | C      | 1   |        |      |       |
|          |       | Germany | atalog |     |        |      |       |
|          | HYE   |         |        |     |        |      |       |
|          | -M55G |         |        |     |        |      |       |
|          |       |         |        |     |        |      |       |
|          | 954-3 |         |        |     |        |      |       |
|          | fib   |         |        |     |        |      |       |
|          | erite |         |        |     |        |      |       |
+----------+-------+---------+--------+-----+--------+------+-------+
| Tracker  | C     | ADCO,   | ADCO   | N   | Note 4 | None | Note  |
| Conical  | arbon | Aachen  |        | ote |        |      | 5     |
|          | fiber |         | C      | 1   |        |      |       |
| flange   |       | Germany | atalog |     |        |      |       |
|          | M55J  |         |        |     |        |      |       |
|          | CE3   |         |        |     |        |      |       |
+----------+-------+---------+--------+-----+--------+------+-------+

Notes:

1\) Manufacturers Certificate of Conformity are available

2\) Flatwise tensile test on Sandwich facing, traction tests at 90 deg,

3\) Insert tests to validate modification of tracker planes, Contraves
Report No. W-ET 99.11.15-1, 15 November 1999

4\) NDE tests include Electrical continuity tests, Insert proof load
test and Interface geometry measurement (Metrology)

5\) Damage control will be implemented by careful handling and
inspection to assure quality of the hardware

+---------+--------+---------+----------+-----+------+-----+-------+
| **F     |        |         |          |     |      |     |       |
| racture |        |         |          |     |      |     |       |
| Certif  |        |         |          |     |      |     |       |
| ication |        |         |          |     |      |     |       |
| for     |        |         |          |     |      |     |       |
| Star    |        |         |          |     |      |     |       |
| Tracker |        |         |          |     |      |     |       |
| Co      |        |         |          |     |      |     |       |
| mposite |        |         |          |     |      |     |       |
| Struc   |        |         |          |     |      |     |       |
| tures** |        |         |          |     |      |     |       |
+---------+--------+---------+----------+-----+------+-----+-------+
| **Comp  | **Mate | **M     | **Basis  | **  | **N  | **  | **D   |
| onent** | rial** | anufact | for      | Qua | DE** | Sam | amage |
|         |        | urers** | ma       | lit |      | ple | Co    |
|         |        |         | terial** | y** | **   | t   | ntrol |
|         |        | *       |          |     | Tech | est | P     |
|         |        | *Name** | **prop   | **  | niqu | s** | lan** |
|         |        |         | erties** | Con | es** |     |       |
|         |        |         |          | tro |      |     |       |
|         |        |         |          | l** |      |     |       |
+---------+--------+---------+----------+-----+------+-----+-------+
| Upper   | CFRP   | A       | Advanced | N   | Note | N   | Note  |
| support | M55J   | dvanced | Co       | ote | 3    | ote | 7     |
| bracket |        |         | mposites | 1,2 |      | 4   |       |
|         | Fiber  | Com     |          |     |      |     |       |
|         |        | posites | and RIBA |     |      |     |       |
|         | ACG    | UK      |          |     |      |     |       |
|         | LTM110 |         | Co       |     |      |     |       |
|         |        | RIBA    | mposites |     |      |     |       |
|         | C      | Com     |          |     |      |     |       |
|         | yanate | posites | catalog  |     |      |     |       |
|         | Ester  |         |          |     |      |     |       |
|         |        | Italy   |          |     |      |     |       |
|         | resin  |         |          |     |      |     |       |
+---------+--------+---------+----------+-----+------+-----+-------+
| Lower   | CFRP   | A       | Advanced | N   | Note | N   | Note  |
| support | M55J   | dvanced | Co       | ote | 3    | ote | 7     |
| bracket |        |         | mposites | 1,2 |      | 4   |       |
|         | Fiber  | Com     |          |     |      |     |       |
|         |        | posites | and RIBA |     |      |     |       |
|         | ACG    | UK      |          |     |      |     |       |
|         | LTM110 |         | Co       |     |      |     |       |
|         |        | RIBA    | mposites |     |      |     |       |
|         | C      | Com     |          |     |      |     |       |
|         | yanate | posites | catalog  |     |      |     |       |
|         | Ester  |         |          |     |      |     |       |
|         |        | Italy   |          |     |      |     |       |
|         | resin  |         |          |     |      |     |       |
+---------+--------+---------+----------+-----+------+-----+-------+
| Att     | Hysol  | Loctite | Loctite  | N   | Note | N   | Note  |
| achment |        |         |          | ote | 3    | ote | 7     |
|         | EA     | Ae      | Catalog  | 1,2 |      | 4   |       |
| between | 9394   | rospace |          |     |      |     |       |
| upper   |        |         |          |     |      |     |       |
|         |        | Cali    |          |     |      |     |       |
| bracket |        | fornia, |          |     |      |     |       |
| and     |        | USA     |          |     |      |     |       |
|         |        |         |          |     |      |     |       |
| Tracker |        |         |          |     |      |     |       |
| Conical |        |         |          |     |      |     |       |
|         |        |         |          |     |      |     |       |
| Flange  |        |         |          |     |      |     |       |
+---------+--------+---------+----------+-----+------+-----+-------+

Notes

1\) AMICA Star Tracker Support Fracture Control for Composite Parts,
AMS-AST-Q1104-i1, 12 July 2005 AMS-AST-Q1104-i1,12 July, 2005

2\) Certificate of Conformance for all materials are included in Ref. 1,
sect 10.2

3\) NDE tests for all materials include Visual, Ultrasonic and 3d
inspection

4\) Material testing and certification is done. Ref. 2, sect 10

5\) AMICA Star Tracker Support Structure handling procedures, Ref 1 sect
11.4, 11.5

6\) Star Tracker Support Structure venting, ASTS_Venting_040705, July 4,
2005

7\) Damage control will be implemented by careful handling and
inspection t0assure quality of the hardware

+-------+------+---------+------------+----+-------+-------+-------+
| **Fra |      |         |            |    |       |       |       |
| cture |      |         |            |    |       |       |       |
| Cer   |      |         |            |    |       |       |       |
| tific |      |         |            |    |       |       |       |
| ation |      |         |            |    |       |       |       |
| for   |      |         |            |    |       |       |       |
| Ring  |      |         |            |    |       |       |       |
| Im    |      |         |            |    |       |       |       |
| aging |      |         |            |    |       |       |       |
| Che   |      |         |            |    |       |       |       |
| rnkov |      |         |            |    |       |       |       |
| Co    |      |         |            |    |       |       |       |
| unter |      |         |            |    |       |       |       |
| (     |      |         |            |    |       |       |       |
| RICH) |      |         |            |    |       |       |       |
| Comp  |      |         |            |    |       |       |       |
| osite |      |         |            |    |       |       |       |
| St    |      |         |            |    |       |       |       |
| ructu |      |         |            |    |       |       |       |
| res** |      |         |            |    |       |       |       |
+-------+------+---------+------------+----+-------+-------+-------+
| **C   | **Ma | **M     | **Basis    | *  | **    | **S   | **D   |
| ompon | teri | anufact | for        | *Q | NDE** | ample | amage |
| ent** | al** | urers** | material** | ua |       | te    | Co    |
|       |      |         |            | li | **Te  | sts** | ntrol |
|       |      | *       | **pr       | ty | chniq |       | P     |
|       |      | *Name** | operties** | ** | ues** |       | lan** |
|       |      |         |            |    |       |       |       |
|       |      |         |            | *  |       |       |       |
|       |      |         |            | *C |       |       |       |
|       |      |         |            | on |       |       |       |
|       |      |         |            | tr |       |       |       |
|       |      |         |            | ol |       |       |       |
|       |      |         |            | ** |       |       |       |
+-------+------+---------+------------+----+-------+-------+-------+
| Ae    | Pr   | Plyform | Plyform    | No | Note  | None  | Note  |
| rogel | epre |         |            | te | 1,2   |       | 5     |
|       | g-1- | Milan,  | Catalog    | 1  |       |       |       |
| Ra    |      | Italy   |            | ,2 |       |       |       |
| ditor | 4    |         |            |    |       |       |       |
|       | 2%-3 |         |            |    |       |       |       |
|       | KHS- |         |            |    |       |       |       |
|       |      |         |            |    |       |       |       |
|       | P    |         |            |    |       |       |       |
|       | -193 |         |            |    |       |       |       |
+-------+------+---------+------------+----+-------+-------+-------+
| Refl  | B    | Co      | Technical  | No | Note  | Note  | Note  |
| ector | ryte | mposite | data       | te | 3     | 4     | 5     |
|       | M46  | Mirror  | sheets     | 3  |       |       |       |
|       | J    |         |            |    |       |       |       |
|       | /EX- | Appli   |            |    |       |       |       |
|       | 1515 | cations |            |    |       |       |       |
|       |      |         |            |    |       |       |       |
|       | Epi  | Tucson, |            |    |       |       |       |
|       | bond | Arizona |            |    |       |       |       |
|       |      |         |            |    |       |       |       |
|       | 121  |         |            |    |       |       |       |
|       | 0-AB |         |            |    |       |       |       |
+-------+------+---------+------------+----+-------+-------+-------+

Notes:

1\) Quality assurance , Plyform document Carlo Gavazzi Space, 16
December 2004

2\) Plyform Certification of Conformity, 21 February 2005

3\) Certificate of Conformance, CMA document 10025, 8/31/2005, contains
Cof C for all materials, Technical data Visual inspection, Material,
Quality assurance, process information and handling Procedures and
Coordinated Measuring Machine Measurements (CMM).

4\) Micro VCM test per ASTM E-595-90

5\) Damage control will be implemented by careful handling and
inspection to assure quality of the hardware

+--------+-----+----------+------------+-----+-------+--------+------+
| **Fr   |     |          |            |     |       |        |      |
| acture |     |          |            |     |       |        |      |
| C      |     |          |            |     |       |        |      |
| ertifi |     |          |            |     |       |        |      |
| cation |     |          |            |     |       |        |      |
| for    |     |          |            |     |       |        |      |
| ECAL   |     |          |            |     |       |        |      |
| Com    |     |          |            |     |       |        |      |
| posite |     |          |            |     |       |        |      |
| Struct |     |          |            |     |       |        |      |
| ures** |     |          |            |     |       |        |      |
+--------+-----+----------+------------+-----+-------+--------+------+
| *      | **M | *        | **Basis    | **  | **    | **     | **Da |
| *Compo | ate | *Manufac | for        | Qua | NDE** | Sample | mage |
| nent** | ria | turers** | material** | lit |       | t      | Con  |
|        | l** |          |            | y** | **Te  | ests** | trol |
|        |     | **Name** | **pr       |     | chniq |        | Pl   |
|        |     |          | operties** | **  | ues** |        | an** |
|        |     |          |            | Con |       |        |      |
|        |     |          |            | tro |       |        |      |
|        |     |          |            | l** |       |        |      |
+--------+-----+----------+------------+-----+-------+--------+------+
| Honey  | Al  | Capital  | Ma         | N   | Note  | Note 3 | Note |
| comb   | umi | A        | nufacturer | ote | 2     |        | 4    |
|        | num | erospace |            | 1   |       |        |      |
| Panels | c   |          | Catalog    |     |       |        |      |
|        | ore | M        |            |     |       |        |      |
|        |     | achinery |            |     |       |        |      |
|        |     | Corp.    |            |     |       |        |      |
|        |     |          |            |     |       |        |      |
|        |     | Beijing, |            |     |       |        |      |
|        |     | China    |            |     |       |        |      |
+--------+-----+----------+------------+-----+-------+--------+------+

Notes:

1\) Manufacturers Certificate of Conformity will be supplied

2\) Standard Honey comb panel NDE tests

3\) Sample tests done

4\) Damage control will be implemented by careful handling and
inspection to assure quality of the hardware

  --------------- -------------- ------------------- -------------- -------------- -------------- ---------- ----------
  **Fracture                                                                                                 
  Certification                                                                                              
  for Main                                                                                                   
  Radiator                                                                                                   
  Composite                                                                                                  
  Structures**                                                                                               

  **Component**   **Material**   **Manufacturers**   **Basis for    **Quality      **NDE          **Sample   **Damage
                                                     material       Control**      Techniques**   tests**    Control
                                                     Properties**                                            Plan**

  RAM Radiator    Rohacell 52    AIDC Taiwan         AIDC Brochure  Note 1,6       Note 5         Notes      Note 7
  panel sandwich  PMI foam                                                                        2,3,4      
  core                                                                                                       

  RAM Radiator    Rohacell 52    AIDC Taiwan         AIDC Brochure  Note 1,6       Note 5         Notes      Note 7
  panel sandwich  PMI foam                                                                        2,3,4      
  core                                                                                                       
  --------------- -------------- ------------------- -------------- -------------- -------------- ---------- ----------

Notes:

1\) Manufacturers Certificate of Conformity will be supplied

2\) Insert test performed by NASA. Ref report no. 061335, 11 January
2007

3\) Insert test samples produced by Plyform, Italy

4\) Tension and Shear tests are done by NASA. Ref. report no. 061335, 11
January 2007

5\) Fokker Bond test (ultrasonic) on all parts

6\) Incoming inspection (FAW, Resin content) as per ASTM Specification

7\) Damage control will be implemented by careful handling and
inspection to assure quality of the hardware

+---------+-------+-------+-----------+-----+-------+-------+-------+
| **F     |       |       |           |     |       |       |       |
| racture |       |       |           |     |       |       |       |
| Certif  |       |       |           |     |       |       |       |
| ication |       |       |           |     |       |       |       |
| for     |       |       |           |     |       |       |       |
| Tracker |       |       |           |     |       |       |       |
| R       |       |       |           |     |       |       |       |
| adiator |       |       |           |     |       |       |       |
| Co      |       |       |           |     |       |       |       |
| mposite |       |       |           |     |       |       |       |
| Struc   |       |       |           |     |       |       |       |
| tures** |       |       |           |     |       |       |       |
+---------+-------+-------+-----------+-----+-------+-------+-------+
| **Compo | **    | **    | **Basis   | **  | **    | **S   | **D   |
| nents** | Mater | Manuf | for       | Qua | NDE** | ample | amage |
|         | ial** | actur | m         | lit |       | te    | Co    |
|         |       | ers** | aterial** | y** | **Te  | sts** | ntrol |
|         |       |       |           |     | chniq |       | P     |
|         |       | **N   | **pro     | **  | ues** |       | lan** |
|         |       | ame** | perties** | Con |       |       |       |
|         |       |       |           | tro |       |       |       |
|         |       |       |           | l** |       |       |       |
+---------+-------+-------+-----------+-----+-------+-------+-------+
| Ram     | Roh   | AIDC  | AIDC      | N   | Note  | Note  | Note  |
| r       | acell |       |           | ote | 3     | 2     | 7     |
| adiator | 51 IG | T     | Brochure  | 1   |       |       |       |
|         |       | aiwan |           | ,4, |       |       |       |
| Panels  | PMI   |       |           | 5   |       |       |       |
|         | foam  |       |           |     |       |       |       |
| s       |       |       |           |     |       |       |       |
| andwich |       |       |           |     |       |       |       |
| core    |       |       |           |     |       |       |       |
+---------+-------+-------+-----------+-----+-------+-------+-------+
| Wake    | Roh   | AIDC  | AIDC      | N   | Note  | Note  | Note  |
| R       | acell |       |           | ote | 3     | 2     | 7     |
| adiator | 51 IG | T     | Brochure  | 1   |       |       |       |
|         |       | aiwan |           | ,4, |       |       |       |
| Panels  | PMI   |       |           | 5   |       |       |       |
|         | foam  |       |           |     |       |       |       |
| s       |       |       |           |     |       |       |       |
| andwich |       |       |           |     |       |       |       |
| core    |       |       |           |     |       |       |       |
+---------+-------+-------+-----------+-----+-------+-------+-------+
| Att     | CFRP  | Pl    | Plyform   | N   | Note  | Note  | Note  |
| achment |       | yform |           | ote | 6     | 2     | 7     |
|         | Tenax |       | Catalog   | 1   |       |       |       |
| Rods    |       | Italy |           | ,4, |       |       |       |
|         |       |       |           | 5   |       |       |       |
+---------+-------+-------+-----------+-----+-------+-------+-------+

Notes:

1\) Manufacturers Certificate of Conformity will be supplied

2\) Mechanical tests on specimens (prepregs, Joints, adhesives). Tests
done at NASA, 11 January 2007

3\) (A-Scan test for parts produced at AIDC) is done

4\) Raw material conformance certificates are collected

5\) Incoming inspections (FAW, Resin content) as per ASTM specs.

6\) Every piece is tapped and for critical application ultrasonic
resistance (Fokker bond test) is done

7\) Damage control will be implemented by careful handling and
inspection to assure quality of the hardware

+--------+------+---------+-----------+----+-------+-------+-------+
| **Fr   |      |         |           |    |       |       |       |
| acture |      |         |           |    |       |       |       |
| C      |      |         |           |    |       |       |       |
| ertifi |      |         |           |    |       |       |       |
| cation |      |         |           |    |       |       |       |
| for    |      |         |           |    |       |       |       |
| Zenith |      |         |           |    |       |       |       |
| Radi   |      |         |           |    |       |       |       |
| ator** |      |         |           |    |       |       |       |
+--------+------+---------+-----------+----+-------+-------+-------+
| **     | **Ma | **M     | **Basis   | *  | **    | **S   | **D   |
| Compon | teri | anufact | for       | *Q | NDE** | ample | amage |
| ents** | al** | urers** | m         | ua |       | te    | Co    |
|        |      |         | aterial** | li | **Te  | sts** | ntrol |
|        |      | *       |           | ty | chniq |       | P     |
|        |      | *Name** | **pro     | ** | ues** |       | lan** |
|        |      |         | perties** |    |       |       |       |
|        |      |         |           | *  |       |       |       |
|        |      |         |           | *C |       |       |       |
|        |      |         |           | on |       |       |       |
|        |      |         |           | tr |       |       |       |
|        |      |         |           | ol |       |       |       |
|        |      |         |           | ** |       |       |       |
+--------+------+---------+-----------+----+-------+-------+-------+
| Ra     | Roha | Plyform | Plyform   | No | Note  | Note  | Note  |
| diator | cell |         |           | te | 3     | 2, 4  | 5     |
|        | 52   | Italy   | Brochure  | 1  |       |       |       |
| Panels |      |         |           |    |       |       |       |
|        | PMI  |         |           |    |       |       |       |
| Sa     | Foam |         |           |    |       |       |       |
| ndwich |      |         |           |    |       |       |       |
| core   |      |         |           |    |       |       |       |
+--------+------+---------+-----------+----+-------+-------+-------+
| Int    | GFRP | Plyform | Plyform   | No | Note  | None  | Note  |
| erface |      |         |           | te | 3     |       | 5     |
|        |      | Italy   | Brochure  | 1  |       |       |       |
| Spokes |      |         |           |    |       |       |       |
+--------+------+---------+-----------+----+-------+-------+-------+
| Z      | GFRP | Plyform | Plyform   | No | Note  | None  | Note  |
| B      |      |         |           | te | 3     |       | 5     |
| racket |      | Italy   | Brochure  | 1  |       |       |       |
+--------+------+---------+-----------+----+-------+-------+-------+

Notes:

1\) Manufacturers Certificate of Conformity will be supplied

2\) Mechanical tests on specimens (Prepregs, Joints, adhesives). Tests
done at NASA, Ref. Report No. 061335, 11 January 2007

3\) Fokker Bond test (Ultrasonic) on all parts

4\) Tension and shear tests done by NASA, Ref. Report No. 061335, 11
January 2007

5\) Damage control will be implemented by careful handling and
inspection to assure quality of the hardware

+-------+---------+--------+----------+----+-------+-------+-------+
| **Fra |         |        |          |    |       |       |       |
| cture |         |        |          |    |       |       |       |
| Cer   |         |        |          |    |       |       |       |
| tific |         |        |          |    |       |       |       |
| ation |         |        |          |    |       |       |       |
| of    |         |        |          |    |       |       |       |
| Upper |         |        |          |    |       |       |       |
| Time  |         |        |          |    |       |       |       |
| of    |         |        |          |    |       |       |       |
| F     |         |        |          |    |       |       |       |
| light |         |        |          |    |       |       |       |
| Comp  |         |        |          |    |       |       |       |
| osite |         |        |          |    |       |       |       |
| St    |         |        |          |    |       |       |       |
| ructu |         |        |          |    |       |       |       |
| res** |         |        |          |    |       |       |       |
+-------+---------+--------+----------+----+-------+-------+-------+
| **Co  | **Mat   | **Man  | **Basis  | *  | **    | **S   | **D   |
| mpone | erial** | ufactu | for      | *Q | NDE** | ample | amage |
| nts** |         | rers** | ma       | ua |       | te    | Co    |
|       |         |        | terial** | li | **Te  | sts** | ntrol |
|       |         | **     |          | ty | chniq |       | P     |
|       |         | Name** | **prop   | ** | ues** |       | lan** |
|       |         |        | erties** |    |       |       |       |
|       |         |        |          | *  |       |       |       |
|       |         |        |          | *C |       |       |       |
|       |         |        |          | on |       |       |       |
|       |         |        |          | tr |       |       |       |
|       |         |        |          | ol |       |       |       |
|       |         |        |          | ** |       |       |       |
+-------+---------+--------+----------+----+-------+-------+-------+
| S     | Carbon  | RAV    | S.P.     | No |       |       | Note  |
| ensor | fiber   | S.r.l. | Systems  | te |       |       | 3     |
| boxes |         | Italy  | England  | 1  |       |       |       |
+-------+---------+--------+----------+----+-------+-------+-------+
| Sc    | Carbon  | RAV    | S.P.     | No |       |       | Note  |
| intil | fiber   | S.r.l. | Systems  | te |       |       | 3     |
| lator |         | Italy  | England  | 1  |       |       |       |
|       |         |        |          |    |       |       |       |
| cover |         |        |          |    |       |       |       |
+-------+---------+--------+----------+----+-------+-------+-------+
| Sc    | Po      | Eljen  | Eljen    | No |       |       | Note  |
| intil | lyvinil | Tech   | Te       | te |       |       | 3     |
| lator | toluene | nology | chnology | 1  |       |       |       |
|       |         |        |          |    |       |       |       |
| core  |         | Texas  | Catalog  |    |       |       |       |
+-------+---------+--------+----------+----+-------+-------+-------+
| Sc    | Carbon  | RAV    | S.P.     | No |       |       | Note  |
| intil | fiber   | S.r.l. | Systems  | te |       |       | 3     |
| lator |         | Italy  | England  | 1  |       |       |       |
|       |         |        |          |    |       |       |       |
| sup   |         |        |          |    |       |       |       |
| ports |         |        |          |    |       |       |       |
+-------+---------+--------+----------+----+-------+-------+-------+
| PMT   | Polycar | Mec    | Bayer    | No |       |       | Note  |
| boxes | abonato | canica |          | te |       |       | 3     |
|       | M       | T      |          | 1  |       |       |       |
|       | akrolon | ecnica |          |    |       |       |       |
|       | 8325    | Italy  |          |    |       |       |       |
+-------+---------+--------+----------+----+-------+-------+-------+
| PMT   | Polycar | I.     | Bayer    |    |       |       | Note  |
| Sup   | abonato | N.F.N. |          |    |       |       | 3     |
| ports | M       | Italy  |          |    |       |       |       |
|       | akrolon |        |          |    |       |       |       |
|       | clear   |        |          |    |       |       |       |
+-------+---------+--------+----------+----+-------+-------+-------+
| PMT   | Carbon  | RAV    | S.P.     |    |       |       | Note  |
| P     | fiber   | S.r.l. | Systems  |    |       |       | 3     |
| anels | sheet   | Italy  | England  |    |       |       |       |
| su    | Al 5052 |        |          |    |       |       |       |
| pport | core    |        | I        |    |       |       |       |
|       |         |        | .MA.TEC. |    |       |       |       |
|       |         |        | Catalog  |    |       |       |       |
+-------+---------+--------+----------+----+-------+-------+-------+
| Ribs  | Carbon  | RAV    | S.P.     | No |       |       | Note  |
|       | fiber   | S.r.l. | Systems  | te |       |       | 3     |
|       |         | Italy  | England  | 1  |       |       |       |
+-------+---------+--------+----------+----+-------+-------+-------+
| Hone  | 2       | RAV    | I        | No |       |       | Note  |
| ycomb | 024-T81 | S.r.l. | .MA.TEC. | te |       |       | 3     |
|       | facings | Italy  | Catalog  | 1  |       |       |       |
| Panel |         |        |          |    |       |       |       |
|       | Al      |        |          |    |       |       |       |
|       | 5052-Al |        |          |    |       |       |       |
|       | 3003    |        |          |    |       |       |       |
|       | core    |        |          |    |       |       |       |
+-------+---------+--------+----------+----+-------+-------+-------+

Notes:

1\) RAV documentation 19 September 2005 contains certification of
compliance, process information and manufacturing description

2\) NDE techniques

3\) Damage control will be implemented by careful handling and
inspection to assure quality of the hardware

+-------+-----+---------+-----------+------+-------+-------+-------+
| **Fra |     |         |           |      |       |       |       |
| cture |     |         |           |      |       |       |       |
| Cer   |     |         |           |      |       |       |       |
| tific |     |         |           |      |       |       |       |
| ation |     |         |           |      |       |       |       |
| for   |     |         |           |      |       |       |       |
| Anti  |     |         |           |      |       |       |       |
| C     |     |         |           |      |       |       |       |
| oinci |     |         |           |      |       |       |       |
| dence |     |         |           |      |       |       |       |
| Coun  |     |         |           |      |       |       |       |
| ter** |     |         |           |      |       |       |       |
+-------+-----+---------+-----------+------+-------+-------+-------+
| **Co  | **M | **M     | **Basis   | **Q  | **    | **S   | **D   |
| mpone | ate | anufact | for       | uali | NDE** | ample | amage |
| nts** | ria | urers** | m         | ty** |       | te    | Co    |
|       | l** |         | aterial** |      | **Te  | sts** | ntrol |
|       |     | *       |           | **C  | chniq |       | P     |
|       |     | *Name** | **pro     | ontr | ues** |       | lan** |
|       |     |         | perties** | ol** |       |       |       |
+-------+-----+---------+-----------+------+-------+-------+-------+
| ACC   | Car | IKV     | Man       | Note | Note  | None  | Note  |
| cyl   | bon | (I      | ufacturer | 1, 3 | 4     |       | 5     |
| inder | fi  | nstitut | catalog   |      |       |       |       |
|       | ber | fur     |           |      |       |       |       |
|       |     | Kun     |           |      |       |       |       |
|       |     | ststoff |           |      |       |       |       |
|       |     | verar   |           |      |       |       |       |
|       |     | B       |           |      |       |       |       |
|       |     | eitung, |           |      |       |       |       |
|       |     | Aachen, |           |      |       |       |       |
|       |     | Germany |           |      |       |       |       |
+-------+-----+---------+-----------+------+-------+-------+-------+

Notes:

1\) Certificate of Conformance is available

2\) Machining of cylinder at Physikalische Institut RWTH, Aachen,
Germany

3\) Quality control includes Computer controlled filament winding,
curing cycle and mass report

4\) Assembly work at RWTH Aachen has been done in restricted area

5\) Damage control will be implemented by careful handling and
inspection to assure quality of the hardware

  ---------------------------------------- ----------------------------------------------------
  ![](media/image1.png){width="4.0625in"   ![](media/image2.png){width="3.9631944444444445in"
  height="5.678472222222222in"}            height="5.669444444444444in"}

  AMS-02 Composite Straps Creep Assessment 
  ---------------------------------------- ----------------------------------------------------

STRESS CORROSION CRACKING SUSCEPTIBLE MATERIAL APPLICATIONS SUMMARY

  ----------------------------------------------------------------------------------------------
  **Table I:                                                                   
  Listing of SCC                                                               
  Susceptable                                                                  
  Materials Used                                                               
  in Various                                                                   
  Subsystems of                                                                
  AMS-02**                                                                     
  --------------- ------------------------- -------------- ------------------- -----------------
                                                                               

  **Subsystem**   **Part Name/Part Number** **Material**   **Specification**   **SCC Rating**

  USS             Outer Cylinder, Vacuum    AL 7050-T7451  AMS 4108            \"U\" per MAPTIS,
                  Case Assy/ SDG39135779                                       Table II per
                                                                               MSFC-STD-3029

  USS             Lower Support Ring,       AL 7050-T7451  AMS 4108            \"U\" per MAPTIS,
                  Vacuum Case                                                  Table II per
                  Assy/SDG39135785                                             MSFC-STD-3029

  USS             Upper Support Ring,       AL 7050-T7451  AMS 4108            \"U\" per MAPTIS,
                  Vacuum Case Assy/                                            Table II per
                  SDG39135784                                                  MSFC-STD-3029

  USS             Interface Plate Assy,     AL 7050-T7451  AMS 4050            \"U\" per MAPTIS,
                  Upper, VCA/ SDG39135788                                      Table II per
                                                                               MSFC-STD-3029

  USS             Interface Plate Assy,     AL 7050-T7451  AMS 4050            \"U\" per MAPTIS,
                  Lower, VCA/ SDG39135789                                      Table II per
                                                                               MSFC-STD-3029

  USS             Upper Vacuum Case         AL 7050-T7451  BMS 7-323C          \"U\" per MAPTIS,
                  Interface Joint Assy,                                        Table II per
                  Upper USS-02 Assy/                                           MSFC-STD-3029
                  SDG39135727                                                  

  USS             Sill Joint Assy, Upper    AL 7050-T7451  BMS 7-323C          \"U\" per MAPTIS,
                  USS-02 Assy/ SDG39135730                                     Table II per
                                                                               MSFC-STD-3029

  USS             Bridge Beam Elbow, Lower  AL 7050-T7451  BMS 7-323C          \"U\" per MAPTIS,
                  Trunnion/ SDG39135734                                        Table II per
                                                                               MSFC-STD-3029

  USS             Interface Joint Assy,     AL 7050-T7451  BMS 7-323C          \"U\" per MAPTIS,
                  Lower VC, Lower USS-02                                       Table II per
                  Assy/ SDG39135737                                            MSFC-STD-3029

  USS             Bracket, Sill, Upper      AL 7050-T7451  BMS 7-323C          \"U\" per MAPTIS,
                  USS-02 Assy/ SDG39135738                                     Table II per
                                                                               MSFC-STD-3029

  USS             Diagonal Bracket, Sill,   AL 7050-T7451  BMS 7-323C          \"U\" per MAPTIS,
                  Upper USS-02 Assy/                                           Table II per
                  SDG39135740                                                  MSFC-STD-3029

  USS             Centerbody Box Joint Keel AL 7050-T7451  BMS 7-323C          \"U\" per MAPTIS,
                  Interface Assy, Lower                                        Table II per
                  USS-02 Assy/ SDG39135759                                     MSFC-STD-3029

  USS             Centerbody Box Joint      AL 7050-T7451  BMS 7-323C          \"U\" per MAPTIS,
                  Assy, Lower USS-02 Assy/                                     Table II per
                  SDG39135760                                                  MSFC-STD-3029

  USS             Joint Assy, Lower USS to  AL 7050-T7451  BMS 7-323C          \"U\" per MAPTIS,
                  Upper USS, Lower USS-02                                      Table II per
                  Assy/ SDG39135762                                            MSFC-STD-3029

  USS             RICH Mounting Bracket,    AL 7050-T7451  BMS 7-323C          \"U\" per MAPTIS,
                  Lower USS-02 Assy/                                           Table II per
                  SDG39135763                                                  MSFC-STD-3029

  USS             PAS RICH Bracket Assy,    AL 7050-T7451  BMS 7-323C          \"U\" per MAPTIS,
                  Lower USS-02 Assy/                                           Table II per
                  SDG39135766                                                  MSFC-STD-3029

  USS             Lower Angle Beam Flange,  AL 7050-T7451  BMS 7-323C          \"U\" per MAPTIS,
                  Lower USS-02 Assy/                                           Table II per
                  SDG39135767                                                  MSFC-STD-3029

  USS             Keel Angle Joint, Keel    AL 7050-T7451  BMS 7-323C          \"U\" per MAPTIS,
                  Assy/ SDG39135769                                            Table II per
                                                                               MSFC-STD-3029

  USS             Keel Block Assy, Keel     AL 7050-T7451  BMS 7-323C          \"U\" per MAPTIS,
                  Assy/ SDG39135770                                            Table II per
                                                                               MSFC-STD-3029

  USS             PAS Platform Assy, PAS    AL 7050-T7451  BMS 7-323C          \"U\" per MAPTIS,
                  Base Assy/ SDG39135817                                       Table II per
                                                                               MSFC-STD-3029

  USS             Bridge Assy, PAS Bridge   AL 7050-T7451  BMS 7-323C          \"U\" per MAPTIS,
                  Assy/ SDG39135837                                            Table II per
                                                                               MSFC-STD-3029

  USS             UMA Bracket/ SDG39135858  AL 7050-T7451  BMS 7-323C or AMS   \"U\" per MAPTIS,
                                                           4108                Table II per
                                                                               MSFC-STD-3029

  USS             PVGF Bracket/ SDG39135860 AL 7050-T7451  BMS 7-323C or AMS   \"U\" per MAPTIS,
                                                           4108                Table II per
                                                                               MSFC-STD-3029

  USS             FRGF Bracket/ SDG39135861 AL 7050-T7451  BMS 7-323C or AMS   \"U\" per MAPTIS,
                                                           4108                Table II per
                                                                               MSFC-STD-3029

  USS             Scuff Plate/ SDG39135867  AL 7050-T7451  BMS 7-323C or AMS   \"U\" per MAPTIS,
                                                           4108                Table II per
                                                                               MSFC-STD-3029

  RICH            Breather Valve, Aerogel   AL 2011-T3     TBD                 \"C\" per MAPTIS,
                  Container/ RICH-C790RPVXX                                    Table III per
                                                                               MSFC-STD-3029

  Cryomag         AMS-02 Helium Tank/ TBD   AL 5083-H111   TBD                 \"B\" per MAPTIS,
                                                                               Table II per
                                                                               MSFC-STD-3029

  Tracker         Ladder Feet and Inserts/  AL 7075-T6     TBD                 \"C\" per MAPTIS,
                  AMS1101 and AMSII-148                                        Table III per
                                                                               MSFC-STD-3029

  Tracker         Thermal Bars and Bridge   AL 5083-O      TBD                 \"B\" per MAPTIS,
                  Bracketry/ AMSII-179,                                        Table II per
                  AMS2002                                                      MSFC-STD-3029
  ----------------------------------------------------------------------------------------------