<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-F03</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">Cryogenics, Pressure Systems, Structures</td>
<td>e. HAZARD GROUP:</td>
<td colspan="2">Explosion, Injury, Loss of Orbiter Entry Capability</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">Rupture of Superfluid Helium Tank, Vacuum
Case and/or Cryosystem Pressurized System Element</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 ISS Addendum, 200.1, 200.1b, 200.2,
200.3, 200.4a, 201.3, 205, 206, 208.1, 208.2, 208.3, 208.4, 208.4a,
208.4b, 208.4c &amp; 208.4e</td>
</tr>
<tr class="odd">
<td colspan="4">j. DESCRIPTION OF HAZARD:</td>
<td colspan="8"><p>Rupture/Explosion of the vacuum case and/or SFHe
pressure system results in significant damage to/loss of the STS, ISS,
crew and/or other payloads.</p>
<p>NOTE: Other Pressurized Systems, including composite overwrapped
tanks, are addressed in AMS-02-F05</p></td>
</tr>
<tr class="even">
<td>k. CAUSES</td>
<td colspan="11" rowspan="2"><blockquote>
<p>1. Inadequate design strength for pressure and other loading
environments.</p>
<p>2. Improper material selection and processing.</p>
<p>3. Improper workmanship and/or assembly.</p>
<p>4. Propagation of crack-like defects.</p>
<p>5. Liquid freezing/thawing.</p>
<p>6. Improper filling/over filling of vessel/system.</p>
<p>7. Incorrect commanding of valves.</p>
<p>8. Meteoroid and Orbital Debris (M/OD) impact.</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 design strength for pressure and
other loading environments.</td>
<td colspan="2"></td>
</tr>
<tr class="even">
<td colspan="10"><p>1.1 CONTROL: The AMS-02 hardware has been designed
to provide positive margins of safety to the appropriate factors of
safety for the hardware as defined in NSTS 1700.7B and NSTS 1700.7B ISS
Addendum. The MDP for the hardware components have been established
under the worst case environmental conditions and where applicable, two
failure case. Where pressure systems elements also experience mechanical
loads, the combined loads have been used in establishing the positive
margin of safety for the pressurized hardware. (See Control 1.3 for
minor exceptions to compliance of proof testing)</p>
<p>The Vacuum Case and Cryogenic Helium Tank meet a design factor of
safety of 1.5, this does not meet the nominal 2.0 requirement of NSTS
1700.7B ISS Addendum, paragraph 208.4a and has not been accepted under
the alternate provision of the paragraph. Non-compliance will be
processed to this specific requirement with acceptance rationale.</p>
<p>With the exception of Orbiter Maximum Q (approximately T+30 seconds
to T+60 seconds) the Leak Before Burst aspect of the pressure system
components leak is non-hazardous.</p>
<p>1.1.1 SVM: AMS-02 Structural Analysis and Tests as defined in AMS-02
SVP (JSC 28792C).</p>
<p>1.1.2 SVM: LBB Analysis/Fracture Control Assessment</p>
<p>1.1.3 SVM: AMS-02 Non-compliance to NSTS 1700.7B ISS Addendum,
paragraph 208.4a approval</p>
<p>1.1.1 STATUS: Open. MDP for each piece of hardware has been
established. Structural analysis is ongoing.</p>
<p>1.1.2 STATUS: Open</p>
<p>1.1.3 STATUS: Open</p></td>
<td colspan="2"></td>
</tr>
<tr class="odd">
<td colspan="10"><p>1.2 CONTROL: The Cryomagnet system utilizes burst
disks to establish the pressure within discrete volumes within the
Cryomagnet system helium and vacuum vessel volumes, these burst disks
are used to establish the MDP of the systems of the AMS-02 Cryogenic
system. The MDP of the system elements are documented in the attached
table.</p>
<p>The Vacuum Case is constructed of aluminum forgings that are of
welded construction except for the interfaces between the support rings,
conical flanges and outer cylinder and the feed through port interfaces
all which use double o-ring interfaces. The VC is designed to have an
MDP of -14.7 psia and 0.8 bar (11.6 psi). The positive pressure MDP is
protected by multiple burst disks (see below).</p>
<p>The Superfluid Helium Tank is a 2500 liter toroidal vessel which
contains the bulk of the cryogen used by AMS-02. the tank consists of a
central support ring attached to two rib-stiffened cylinders made up of
Al 5083 forgings and all interfaces are welded. Sixteen through tubes
are welded in place to allow for Cryomagnet support straps to pass
through. The tank itself has been designed to a maximum positive
pressure of 3 bar and a maximum negative pressure of 1 bar. The tank
over pressure is protected by multiple burst disks (see below).</p>
<p>The Cryogenic plumbing system is constructed principally of stainless
steel and the MDPs of the various system elements are described in the
attached table. These system segments are ultimately protected by burst
disks installed in the systems that the lines route to or attached to
the lines directly (see below).</p>
<p>All burst disks will meet the requirements for a single failure
tolerant specially certified burst disk per NASA/JSC TA-88-074. The
burst disks implemented are “Reverse Acting Circumferentially Scored
with Cutting Teeth” Burst Disk manufactured by Fike. The burst disks are
designed to open along the scored line upon pressure exceedence. In
addition to the nominal manner of rupture, teeth will tear into the
scoring as the pressure distorts the disk. All burst disks are sized to
individually allow for sufficient flow to preclude pressure build up
based on the worst-case thermal input into the cryogenic system. The
interspace between the burst disks is evacuated to allow for a constant
stress condition while in space. These volumes are evacuated and the
stubs used for this are double crimped and welded. Burst disk
installation/manufacture provides sealing against leakage past burst
disk into the interspace between burst disks.</p>
<p>1.2.1 SVM: Review of design</p>
<p>1.2.2 SVM: Inspection of as built hardware.</p>
<p>1.2.3 SVM: Qualification of Burst Disks (as described in attached
memos)</p>
<p>1.2.4 SVM: Qualification of the evacuation port crimping and welding
process.</p>
<p>1.2.5 SVM: Vacuum Case Testing/Analysis</p>
<p>1.2.6 SVM: Qualification/Acceptance testing/analysis of Helium
Tank</p>
<p>1.2.7 SVM: Qualification/Acceptance testing/analysis of Cryogenic
Plumbing System.</p>
<p>1.2.8 SVM: Qualification/Acceptance testing of series burst disks to
assure no leakage potential into interspace volumes (including
MV33A&amp;B and cap), review of result by EP4.</p>
<p>1.2.1 STATUS: Open</p>
<p>1.2.2 STATUS: Open</p>
<p>1.2.3 STATUS: Open. Burst disk qualification plan described in Space
Cryomagnetics Limited (SCL) Memo #2484, under review by EP4.</p>
<p>1.2.4 STATUS: Open. Memo from Scientific Magnetics outlines
qualification procedure (Memo Ref 2837, “Proposed Qualification
Procedure for Burst Disc Crimping”, dated January 12, 2006.)</p>
<p>1.2.5 STATUS: Open</p>
<p>1.2.6 STATUS: Open</p>
<p>1.2.7 STATUS: Open</p>
<p>1.2.8 STATUS: Open</p></td>
<td colspan="2"></td>
</tr>
<tr class="even">
<td colspan="10"><p>1.3 CONTROL: Sensitive components on the Cryosystem
preclude testing to the nominal 1.5 margin over MDP. These components
will experience deformation or material property changes that affect
mission success but not safety at these pressures. Specifically Weka
heliomatic valve’s activation bellows will distort and thermal
properties of the superfluid cooling loop and cold heat exchanger as the
annealed metals are work hardened. For these limited
components/assemblies, a proof test to 1.1 x MDP will be
accomplished.</p>
<p>1.3.1 SVM: Review of AMS-02 Cryosystem Pressure System Proof Test
Plan,</p>
<p>1.3.1 STATUS: Closed. Proof Testing of AMS-02 Pressure System Test
Plan, Space Cryomagnetics, Issue 01, Dated February 15, 2007</p></td>
<td colspan="2"></td>
</tr>
<tr class="odd">
<td colspan="10">NOTE: Valve DV02 within the Superfluid Cooling Loop
(SCL) is utilized only on the ground and is not operated during launch.
DV02 seals the Superfluid Cooling Loop (SCL) from the filling line. For
ground processing the filling line is connected to a clean, ambient
temperature helium supply. For the entire cool down process (from
ambient temperature to 2.3 K) valve DV02 is open, so that the SCL is
connected to the warm supply. Clean helium is drawn into the SCL
throughout the cool down process: when the temperature of the main
helium tank and coils is below 4.2 K it will condense. Once the
temperature is below 2.3 K, DV02 is closed to seal the SCL. The filling
line (between DV02 and the ambient helium supply) is evacuated. DV02
will never be opened again, unless there is a need to warm up the
Cryomagnet on the ground. If the Cryomagnet is warmed up, the filling
line will again be connected to the ambient helium supply, and DV02 will
be opened for the duration of the warm up. BD 18 protects the segment of
the Super Fluid Cooling Loop during ground operations from an entrapped
volume that could occur during filling or emptying procedure.</td>
<td colspan="2"></td>
</tr>
<tr class="even">
<td colspan="10">2. CAUSE: Improper material selection and
processing.</td>
<td colspan="2"></td>
</tr>
<tr class="odd">
<td colspan="10"><p>2.1 CONTROL: All AMS-02 pressure system materials
are selected to meet the requirements of MSFC-STD-3029 for Stress
Corrosion Cracking. Materials with high resistance to stress corrosion
cracking will be used where possible. If materials with moderate or low
resistance to stress corrosion cracking have to be used, MUAs will be
generated and submitted for approval.</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 CONTROL: The wetted parts of the SFHe pressure
system are made of stainless steel, aluminum or copper, these materials
will not react with He (Inert gas/liquid).</p>
<p>2.2.1 SVM: Material Compatibility Assessment/ JSC ES4/Materials and
Processes Branch Material Certification Letter.</p>
<p>2.2.1 STATUS: Open</p></td>
<td colspan="2"></td>
</tr>
<tr class="odd">
<td colspan="10"><p>2.3 CONTROLS: Cleaning materials will be compatible
with working fluid and materials of construction.</p>
<p>2.3.1 SVM: Materials Compatibility Assessment/Review JSC
ES4/Materials and Processes Branch Material Certification</p>
<p>2.3.1 STATUS: Open</p></td>
<td colspan="2"></td>
</tr>
<tr class="even">
<td colspan="10"><p>2.4 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>2.4.1 SVM: Material Compatibility Assessment</p>
<p>2.4.2 SVM: Approval of material use and MUAs by JSC ES4/Materials and
Processes Branch</p>
<p>2.4.1 STATUS: Open</p>
<p>2.4.2 STATUS: Open</p></td>
<td colspan="2"></td>
</tr>
<tr class="odd">
<td colspan="10">3. CAUSE: Improper workmanship and/or assembly.</td>
<td colspan="2"></td>
</tr>
<tr class="even">
<td colspan="10"><p>3.1 CONTROL: Approved drawings and procedures will
be used for manufacturing and assembly.</p>
<p>3.1.1 SVM: Each supplier of hardware will provide a certificate of
compliance (C of C) to AMS-02 Project. Project will Review and Accept
each of the C of Cs.</p>
<p>3.1.1 STATUS: Open</p></td>
<td colspan="2"></td>
</tr>
<tr class="odd">
<td colspan="10"><p>3.2 CONTROL: Welding Processes are controlled by
implementation of the AMS-02 Weld Control Plans.</p>
<p>3.2.1 SVM: Review and approval of AMS-02 Weld Control Plans by
ES4/Materials and Processes Branch.</p>
<p>3.2.2 SVM: Welds will be inspected: Dye Penetrant, Ultrasound or
X-ray</p>
<p>3.2.1 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>3.2.2 STATUS: Open</p></td>
<td colspan="2"></td>
</tr>
<tr class="even">
<td colspan="10"><p>3.3 CONTROL: All welds have a positive margin of
safety for all mission phases, environmental factors and credible load
combinations as documented in the AMS-02 Structural Verification Plan
(SVP), JSC 28792C.</p>
<p>3.3.1 SVM: AMS-02 Structural Analysis and Tests as defined in AMS-02
SVP (JSC 28792C).</p>
<p>3.3.1 STATUS: Open</p></td>
<td colspan="2"></td>
</tr>
<tr class="odd">
<td colspan="10">4. CAUSE: Propagation of crack-like defects.</td>
<td colspan="2"></td>
</tr>
<tr class="even">
<td colspan="10"><p>4.1 CONTROL: The AMS-02 has implemented fracture
control by using JSC 25863A and implemented in accordance with fracture
control requirements of NASA-STD-5003 and SSP 30558C. All pressurized
components of the Superfluid Helium Tank, Vacuum Case and associated
pressurized system have been shown to be Leak Before Burst and
non-hazardous leak (except during the T+30 to T+60 seconds during
ascent).</p>
<p>4.1.1 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>4.1.1 STATUS: Open</p></td>
<td colspan="2"></td>
</tr>
<tr class="odd">
<td colspan="10">5. CAUSE: Liquid freezing/thawing.</td>
<td colspan="2"></td>
</tr>
<tr class="even">
<td colspan="10"><p>5.1 CONTROL: The freezing of helium is precluded by
the physical property that liquid helium cannot be frozen unless under
the compression of approximately 25 atmospheres. The design of the
Cryomagnet precludes pressure and temperature conditions that can result
in helium freezing. The highest burst value for bursts disks used on the
AMS-02 is 23 bar (22.7 atm).</p>
<p>5.1.1 SVM: Review of design</p>
<p>5.1.2 SVM: Inspection of as built hardware.</p>
<p>5.1.1 STATUS: CLOSED. Review has been conducted independently by
AMS-02 Chief Engineer and documented in memorandum
ESCG-4390-06-SP-MEMO-002, “Freezing of Helium within AMS-02” prepared by
Chris Tutt on December 8, 2005.</p>
<p>5.1.2 STATUS: Open</p></td>
<td colspan="2"></td>
</tr>
<tr class="odd">
<td colspan="10"><p>5.2 CONTROL: During pre-launch operations a vent
pump is the only nominally open path for atmosphere entering the
plumbing of the Cryosystem that doesn’t involve opening valves or
bursting disks is through the line to the porous plug (Possible paths
through DV09A&amp;B, DV15 A-D, MV34A&amp;B). This vent pump is operating
during the preflight condition and will be extracting helium, precluding
the introduction of the atmosphere. Just prior to launch the valve to
the pump is closed (DV09A&amp;B)and the pump’s operation ceases. Once
atmospheric pressure in the payload bay is less than the pressure of the
main helium tank based on a baroswitch operation between 5 mbar (0.04
psia) and 15 mbar (0.12 psia), valves DV15A-D are opened. With these
valves open a positive flow of helium out of the plumbing resumes.
Atmosphere cannot enter the cryosystem.</p>
<p>Note: These valves are opened at this time to avoid a specific
condition where all superfluid helium could be lost in a relatively
short period of time in comparison with the nominal mission time. This
is a mission success concern, not safety. This condition is caused by
the unique properties of the superfluid helium. For return all valves
will be closed (mission success, not safety critical.)</p>
<p>5.2.1 SVM: Review of design</p>
<p>5.2.2 SVM: Inspection of as built hardware</p>
<p>5.2.3 SVM: Review of ground pre-launch procedures.</p>
<p>5.2.4 SVM: Functional testing of pump and valves.</p>
<p>5.2.1 STATUS: Open. Memo ESCG-4390-06-SP-MEMO-0004, “Cryosystem
External Interfaces” Dated 6 March 2006, from AMS-02 Chief Engineer
Chris Tutt.</p>
<p>5.2.2 STATUS: Open</p>
<p>5.2.3 STATUS: Open</p>
<p>5.2.4 STATUS: Open</p></td>
<td colspan="2"></td>
</tr>
<tr class="even">
<td colspan="10">6. CAUSE: Improper filling/over filling of
vessel/system</td>
<td colspan="2"></td>
</tr>
<tr class="odd">
<td colspan="10"><p>6.1 CONTROL: Ground servicing procedures and
hardware will provide high purity helium in gaseous and liquid form (at
4.2 K liquid helium is quite pure). Ground procedures will purge,
evacuate and/or filter all other gases during the cool down and fill
procedures.</p>
<p>6.1.1 SVM: Implement procurement of appropriate quality gases, QA
certification of received gases.</p>
<p>6.1.2 SVM: Review of ground filling procedures.</p>
<p>6.1.3 SVM: QA Approval of procedure implementation.</p>
<p>6.1.1 STATUS: Open</p>
<p>6.1.2 STATUS: Open</p>
<p>6.1.2 STATUS: Open</p></td>
<td colspan="2"></td>
</tr>
<tr class="even">
<td colspan="10">7. CAUSE: Incorrect commanding of valves.</td>
<td colspan="2"></td>
</tr>
<tr class="odd">
<td colspan="10"><p>7.1 CONTROL: All valve pairs with the exception of
valve pairs in gaseous vent paths have a pressure relief device (burst
disk) where any volume of cold gas or liquid may become trapped. The
small segments between valve pairs in the gaseous vents have been
assessed based on worst case thermal conditions and MDPs established
accordingly.</p>
<p>7.1.1 SVM: Review of design</p>
<p>7.1.2 SVM: Inspection of as built hardware.</p>
<p>7.1.3 SVM: Analysis/Testing of pressurized components per SVP</p>
<p>7.1.1 STATUS: Open</p>
<p>7.1.2 STATUS: Open</p>
<p>7.1.3 STATUS: Open</p></td>
<td colspan="2"></td>
</tr>
<tr class="even">
<td colspan="10">8. CAUSE: Meteoroid and Orbital Debris (M/OD)
Impact</td>
<td colspan="2"></td>
</tr>
<tr class="odd">
<td colspan="10"><p>8.1 CONTROL: The AMS-02 is designed to meet the
probability of non-penetration (PNP) requirements of SSP 52005. While
the AMS-02 will have an extended on-orbit life, the pressurized tanks
(Helium Dewar specifically) will only represent a hazardous condition
for a limited period of time before the pressure reserves are spent.
Each tank will be assessed for PNP for the duration of operational life.
The tank is surrounded by the vacuum case and 120 layers of MLI, four
vapor shields and the vacuum case.</p>
<p>8.1.1 SVM: M/OD Risk Assessment to establish a PNP in accordance with
SSP 52005.</p>
<p>8.1.2 SVM: Hypervelocity impact testing on sample materials of
construction (Vacuum case, MLI, vapor cooled shields and the SFHe tank)
to verify tank not susceptible to M/OD impact per SSP 52005.</p>
<p>8.1.3 SVM: Analysis of AMS-02 pressurized system utilization to
establish on-orbit penetration threat life duration (period during which
M/OD represents a hazard to the pressure vessel.)</p>
<p>8.1.1 STATUS: Open. Preliminary Report Complete.</p>
<p>8.1.2 STATUS: Open.</p>
<p>8.1.3 STATUS: Open.</p></td>
<td colspan="2"></td>
</tr>
<tr class="even">
<td colspan="10"><p>Notes:</p>
<p>Helium Boiling Point 4.2 K</p></td>
<td colspan="2"></td>
</tr>
</tbody>
</table>

  -----------------------------------------------------------------------
  ACRONYMS                           
  ---------------------------------- ------------------------------------
  AMS-02 -- Alpha Magnetic           Ops -- Operations
  Spectrometer 02                    

  atm -- atmospheres                 PGSC -- Payload General Support
                                     Computer

  C of C -- Certificate of           psia -- pounds per square inch
  Compliance                         absolute

  CDC -- Cool Down Circuit           psid -- pounds per square inch
                                     differential

  CHX -- Cold Heat Exchanger         QA -- Quality Assurance

  DLCM - Direct Liquid Content       RTEF - RaceTrack End Frame
  Measurement (= mass gauge)         

  He -- Helium                       SCL -- Space Cryomagnetics Limited

  K -- Kelvin                        SCL -- Superfluid Cooling Loop

  ksi -- kilo pounds per square inch SFHe -- Superfluid Helium

  lbf -- pound force                 STA -- Structural Test Article

  M/OD -- Meteoroid/Orbital Debris   SVM -- Safety Verification Method

  mbar -- millibar                   SVP -- Safety Verification Plan

  MDP -- Maximum Design Pressure     TBD -- To Be Done, To Be Determined

  MUA -- Material Usage Agreements   ult -- Ultimate
  -----------------------------------------------------------------------

# CRYOSYSTEM Pressure Table (Including Warm Helium Gas Supply Hardware Addressed in AMS-02-F05)

<table style="width:100%;">
<colgroup>
<col style="width: 7%" />
<col style="width: 8%" />
<col style="width: 8%" />
<col style="width: 7%" />
<col style="width: 5%" />
<col style="width: 6%" />
<col style="width: 6%" />
<col style="width: 9%" />
<col style="width: 4%" />
<col style="width: 5%" />
<col style="width: 8%" />
<col style="width: 5%" />
<col style="width: 6%" />
<col style="width: 10%" />
</colgroup>
<thead>
<tr class="header">
<th><strong>Description</strong></th>
<th><strong>Volume</strong></th>
<th><p><strong>Operating</strong></p>
<p><strong>Pressure</strong></p></th>
<th><p><strong>Material</strong></p>
<p><strong>(See Note 2)</strong></p></th>
<th><strong>Temp</strong></th>
<th><strong>MDP</strong></th>
<th><p><strong>MDP</strong></p>
<p><strong>Determin-ation</strong></p></th>
<th><p><strong>Burst</strong></p>
<p><strong>Pressure</strong></p></th>
<th colspan="2"><p><strong>Burst</strong></p>
<p><strong>Safety Factor</strong></p></th>
<th><p><strong>Proof</strong></p>
<p><strong>Pressure</strong></p></th>
<th><p><strong>Proof</strong></p>
<p><strong>SF</strong></p></th>
<th><p><strong>Basis</strong></p>
<p><strong>(See</strong></p>
<p><strong>Note 3)</strong></p></th>
<th><p><strong>Reference</strong></p>
<p><strong>Document</strong></p></th>
</tr>
<tr class="odd">
<th><strong>Units</strong></th>
<th><p><strong>Liter</strong></p>
<p><strong>(in^3)</strong></p></th>
<th><p><strong>Bar</strong></p>
<p><strong>(psid)</strong></p></th>
<th></th>
<th><strong>(K)</strong></th>
<th><p><strong>Bar</strong></p>
<p><strong>(psid)</strong></p></th>
<th></th>
<th><p><strong>Bar</strong></p>
<p><strong>(psid)</strong></p></th>
<th><strong>Reqd</strong></th>
<th><strong>Actual</strong></th>
<th><p><strong>Bar</strong></p>
<p><strong>(psid)</strong></p></th>
<th></th>
<th><p><strong>A:Analysis</strong></p>
<p><strong>T:Test</strong></p></th>
<th></th>
</tr>
</thead>
<tbody>
<tr class="odd">
<td>Super Fluid Helium Vessel</td>
<td><p>2455</p>
<p>(~150,000)</p></td>
<td><p>0.016</p>
<p>(0.23)</p></td>
<td><p>5083-H321,</p>
<p>H-111</p></td>
<td>1.8</td>
<td>3 (43.5)</td>
<td>See Note 1</td>
<td>&gt;4.5 (65.25)</td>
<td>1.5</td>
<td>1.5</td>
<td>3.3 (47.85)</td>
<td>1.1</td>
<td>T</td>
<td><p>MIL-STD-1522A</p>
<p>SSP 30559C – Bieri Engineering Report No. 450-0</p></td>
</tr>
<tr class="even">
<td>Vacuum Case</td>
<td><p>~2295</p>
<p>(~140,000)</p>
<p>effective volume</p></td>
<td>-1 (-14.5)</td>
<td><p>2219-T62</p>
<p>7050-T7451</p>
<p>2219-T852</p></td>
<td>300</td>
<td><p>0.8</p>
<p>(11.6)</p>
<p>See</p>
<p>Note 4</p></td>
<td>See Note 5</td>
<td>1.2 (17.4)</td>
<td>1.5</td>
<td>1.5</td>
<td>0.8 (11.6)</td>
<td>1</td>
<td>T</td>
<td><p>MIL-STD-1522A</p>
<p>SSP 30559C</p></td>
</tr>
<tr class="odd">
<td>Tube from Helium Vessel to DV07</td>
<td><p>&lt;10</p>
<p>(&lt;610)</p></td>
<td>0.2 (2.9)</td>
<td><p>AISI 316 L</p>
<p>AISI 316 L</p></td>
<td><p>1.8</p>
<p>300</p></td>
<td><p>3 (43.5)</p>
<p>3 (43.5)</p></td>
<td>See Note 1</td>
<td><p>2364 (34278)</p>
<p>946 (13717)</p></td>
<td><p>4</p>
<p>4</p></td>
<td><p>788</p>
<p>315</p></td>
<td><p>4.5 (65.3)</p>
<p>4.5 (65.3)</p></td>
<td><p>1.5</p>
<p>1.5</p></td>
<td><p>A</p>
<p>A</p></td>
<td><p>MIL-STD-1522A</p>
<p>SSP 30559C</p></td>
</tr>
<tr class="even">
<td>Tube from TMP02 to DV14</td>
<td><p>&lt;10</p>
<p>(&lt;610)</p></td>
<td>0.2 (2.9)</td>
<td><p>AISI 316 L</p>
<p>AISI 316 L</p></td>
<td><p>1.8</p>
<p>300</p></td>
<td><p>3 (43.5)</p>
<p>3 (43.5)</p></td>
<td>See Note 1</td>
<td><p>1368 (19836)</p>
<p>547 (7931.5)</p></td>
<td><p>4</p>
<p>4</p></td>
<td><p>456</p>
<p>183</p></td>
<td><p>4.5 (65.3)</p>
<p>4.5 (65.3)</p></td>
<td><p>1.5</p>
<p>1.5</p></td>
<td><p>A</p>
<p>A</p></td>
<td><p>MIL-STD-1522A</p>
<p>SSP 30559C</p></td>
</tr>
<tr class="odd">
<td>Tube from DV14 to T-Junction with CDC</td>
<td><p>&lt;10</p>
<p>(&lt;610)</p></td>
<td>0.2 (2.9)</td>
<td><p>AISI 316 L</p>
<p>AISI 316 L</p></td>
<td><p>1.8</p>
<p>300</p></td>
<td><p>11 (159.5)</p>
<p>11 (159.5)</p></td>
<td>See Note 1</td>
<td><p>1368 (19836)</p>
<p>547 (7931.5)</p></td>
<td><p>4</p>
<p>4</p></td>
<td><p>124</p>
<p>50</p></td>
<td><p>16.5 (239.3)</p>
<p>16.5 (239.3)</p></td>
<td><p>1.5</p>
<p>1.5</p></td>
<td><p>A</p>
<p>A</p></td>
<td><p>MIL-STD-1522A</p>
<p>SSP 30559C</p></td>
</tr>
<tr class="even">
<td><p>Cool Down Circuit</p>
<p>(CDC)</p></td>
<td><p>&lt;10</p>
<p>(&lt;610)</p></td>
<td>0.2 (2.9)</td>
<td><p>AISI 316 L</p>
<p>AISI 316 L</p></td>
<td><p>1.8</p>
<p>300</p></td>
<td><p>11 (159.5)</p>
<p>11 (159.5)</p></td>
<td>See Note 1</td>
<td><p>963 (13963)</p>
<p>385 (5582)</p></td>
<td><p>4</p>
<p>4</p></td>
<td><p>88</p>
<p>35</p></td>
<td><p>16.5 (239.3)</p>
<p>16.5 (239.3)</p></td>
<td><p>1.5</p>
<p>1.5</p></td>
<td><p>A</p>
<p>A</p></td>
<td><p>MIL-STD-1522A</p>
<p>SSP 30559C</p></td>
</tr>
<tr class="odd">
<td>Flexible pipe on exit of CDC</td>
<td><p>&lt;10</p>
<p>(&lt;610)</p></td>
<td>0.2 (2.9)</td>
<td><p>AISI 316 L</p>
<p>AISI 316 L</p></td>
<td><p>1.8</p>
<p>300</p></td>
<td><p>11 (159.5)</p>
<p>11 (159.5)</p></td>
<td>See Note 1</td>
<td><p>&gt;44 (&gt;638)</p>
<p>&gt;44 (&gt;638)</p></td>
<td><p>4</p>
<p>4</p></td>
<td><p>&gt;4</p>
<p>&gt;4</p></td>
<td><p>16.5 (239.3)</p>
<p>16.5 (239.3)</p></td>
<td><p>1.5</p>
<p>1.5</p></td>
<td><p>T</p>
<p>To Be Done) (TBD)</p></td>
<td><p>MIL-STD-1522A</p>
<p>SSP 30559C</p></td>
</tr>
<tr class="even">
<td><p>Superfluid Cooling Loop</p>
<p>(SCL)</p></td>
<td><p>&lt;10</p>
<p>(&lt;610)</p></td>
<td><p>1</p>
<p>(14.5)</p></td>
<td><p>CU 103</p>
<p>AISI 316L</p>
<p>CU 103</p>
<p>AISI 316L</p></td>
<td><p>1.8</p>
<p>1.8</p>
<p>300</p>
<p>300</p></td>
<td><p>23 (333.5)</p>
<p>23 (333.5)</p>
<p>20 (290)</p>
<p>20 (290)</p></td>
<td>See Note 1</td>
<td><p>422 (6203)</p>
<p>908 (13348)</p>
<p>211 (3102)</p>
<p>291 (4278)</p></td>
<td><p>4</p>
<p>4</p>
<p>4</p>
<p>4</p></td>
<td><p>18.3</p>
<p>39.5</p>
<p>10.5</p>
<p>14.5</p></td>
<td><p>34.5 (500)</p>
<p>34.5 (500)</p>
<p>30.0 (435)</p>
<p>30.0 (435)</p></td>
<td><p>1.5</p>
<p>1.5</p>
<p>1.5</p>
<p>1.5</p></td>
<td><p>A</p>
<p>A</p>
<p>A</p>
<p>A</p></td>
<td><p>MIL-STD-1522A</p>
<p>SSP 30559C</p></td>
</tr>
<tr class="odd">
<td>Tube from Helium Vessel to BD02</td>
<td><p>&lt;10</p>
<p>(&lt;610)</p></td>
<td><p>0.016</p>
<p>(0.23)</p></td>
<td><p>AISI 316 L</p>
<p>AISI 316 L</p></td>
<td><p>1.8</p>
<p>300</p></td>
<td><p>3 (43.5)</p>
<p>3 (43.5)</p></td>
<td>See Note 1</td>
<td><p>742 (10759)</p>
<p>297 (4306)</p></td>
<td><p>4</p>
<p>4</p></td>
<td><p>247</p>
<p>99</p></td>
<td><p>4.5 (65.2)</p>
<p>4.5 (65.2)</p></td>
<td><p>1.5</p>
<p>1.5</p></td>
<td>T (TBD)</td>
<td><p>MIL-STD-1522A</p>
<p>SSP 30559C</p></td>
</tr>
<tr class="even">
<td>Tube from BD02 to T-Junction</td>
<td><p>&lt;10</p>
<p>(&lt;610)</p></td>
<td><p>1</p>
<p>(14.5)</p></td>
<td><p>AISI 316 L</p>
<p>AISI 316 L</p></td>
<td><p>1.8</p>
<p>300</p></td>
<td><p>23 (333.5)</p>
<p>20 (290)</p></td>
<td>See Note 1</td>
<td><p>742 (10759)</p>
<p>297 (4306)</p></td>
<td><p>4</p>
<p>4</p></td>
<td><p>32</p>
<p>14</p></td>
<td><p>34.5 (500)</p>
<p>30.0 (435)</p></td>
<td><p>1.5</p>
<p>1.5</p></td>
<td>T (TBD)</td>
<td><p>MIL-STD-1522A</p>
<p>SSP 30559C</p></td>
</tr>
<tr class="odd">
<td>SCL Stainless Tube</td>
<td><p>&lt;10</p>
<p>(&lt;610)</p></td>
<td><p>1</p>
<p>(14.5)</p></td>
<td><p>AISI 316 L</p>
<p>AISI 316 L</p></td>
<td><p>1.8</p>
<p>300</p></td>
<td><p>23 (333.5)</p>
<p>20 (290)</p></td>
<td>See Note 1</td>
<td><p>742 (10759)</p>
<p>297 (4306)</p></td>
<td><p>4</p>
<p>4</p></td>
<td><p>32</p>
<p>14</p></td>
<td><p>34.5 (500)</p>
<p>30.0 (435)</p></td>
<td><p>1.5</p>
<p>1.5</p></td>
<td>T (TBD)</td>
<td><p>MIL-STD-1522A</p>
<p>SSP 30559C</p></td>
</tr>
<tr class="even">
<td>SCL Copper Tube</td>
<td><p>&lt;10</p>
<p>(&lt;610)</p></td>
<td><p>1</p>
<p>(14.5)</p></td>
<td><p>C110 OFHC Copper</p>
<p>C110 OFHC Copper</p></td>
<td><p>1.8</p>
<p>300</p></td>
<td><p>23 (333.5)</p>
<p>20 (290)</p></td>
<td>See Note 1</td>
<td><p>520 (7540)</p>
<p>260 (3770)</p></td>
<td><p>4</p>
<p>4</p></td>
<td><p>22</p>
<p>13</p></td>
<td><p>34.5 (500)</p>
<p>30.0 (435)</p></td>
<td><p>1.5</p>
<p>1.5</p></td>
<td>T (TBD)</td>
<td><p>MIL-STD-1522A</p>
<p>SSP 30559C</p></td>
</tr>
<tr class="odd">
<td>Tube from SCL Junction to DV02a</td>
<td><p>&lt;10</p>
<p>(&lt;610)</p></td>
<td><p>1</p>
<p>(14.5)</p></td>
<td><p>AISI 316 L</p>
<p>AISI 316 L</p></td>
<td><p>1.8</p>
<p>300</p></td>
<td><p>23 (333.5)</p>
<p>20 (290)</p></td>
<td>See Note 1</td>
<td><p>1368 (19836)</p>
<p>547 (7931)</p></td>
<td><p>4</p>
<p>4</p></td>
<td><p>59</p>
<p>27</p></td>
<td><p>34.5 (500)</p>
<p>30.0 (435)</p></td>
<td><p>1.5</p>
<p>1.5</p></td>
<td>T (TBD)</td>
<td><p>MIL-STD-1522A</p>
<p>SSP 30559C</p></td>
</tr>
<tr class="even">
<td>Tube from DV02a to T-Junction with DV02b</td>
<td><p>&lt;10</p>
<p>(&lt;610)</p></td>
<td><p>1</p>
<p>(14.5)</p></td>
<td><p>AISI 316 L</p>
<p>AISI 316 L</p></td>
<td><p>1.8</p>
<p>300</p></td>
<td><p>21 (304)</p>
<p>20 (290)</p></td>
<td>See Note 1</td>
<td><p>1368 (19836)</p>
<p>547 (7931)</p></td>
<td><p>4</p>
<p>4</p></td>
<td><p>65</p>
<p>27</p></td>
<td><p>34.5 (500)</p>
<p>30.0 (435)</p></td>
<td><p>1.5</p>
<p>1.5</p></td>
<td>T (TBD)</td>
<td><p>MIL-STD-1522A</p>
<p>SSP 30559C</p></td>
</tr>
<tr class="odd">
<td>Tube from T-Junction to DV02b</td>
<td><p>&lt;10</p>
<p>(&lt;610)</p></td>
<td><p>1</p>
<p>(14.5)</p></td>
<td><p>AISI 316 L</p>
<p>AISI 316 L</p></td>
<td><p>1.8</p>
<p>300</p></td>
<td><p>21 (304)</p>
<p>20 (290)</p></td>
<td>See Note 1</td>
<td><p>1368 (19836)</p>
<p>547 (7931)</p></td>
<td><p>4</p>
<p>4</p></td>
<td><p>65</p>
<p>27</p></td>
<td><p>34.5 (500)</p>
<p>30.0 (435)</p></td>
<td><p>1.5</p>
<p>1.5</p></td>
<td>T (TBD)</td>
<td><p>MIL-STD-1522A</p>
<p>SSP 30559C</p></td>
</tr>
<tr class="even">
<td>Tube from T-Junction to BD18</td>
<td><p>&lt;10</p>
<p>(&lt;610)</p></td>
<td><p>1</p>
<p>(14.5)</p></td>
<td><p>AISI 316 L</p>
<p>AISI 316 L</p></td>
<td><p>1.8</p>
<p>300</p></td>
<td><p>21 (304)</p>
<p>20 (290)</p></td>
<td>See Note 1</td>
<td><p>1368 (19836)</p>
<p>547 (7931)</p></td>
<td><p>4</p>
<p>4</p></td>
<td><p>65</p>
<p>27</p></td>
<td><p>34.5 (500)</p>
<p>30.0 (435)</p></td>
<td><p>1.5</p>
<p>1.5</p></td>
<td>T (TBD)</td>
<td><p>MIL-STD-1522A</p>
<p>SSP 30559C</p></td>
</tr>
<tr class="odd">
<td>Tube from T-Junction with BD18 and DV02B to bellows for SCL
exit</td>
<td><p>&lt;10</p>
<p>(&lt;610)</p></td>
<td><p>1</p>
<p>(14.5)</p></td>
<td><p>AISI 316 L</p>
<p>AISI 316 L</p></td>
<td><p>1.8</p>
<p>300</p></td>
<td><p>11 (159.5)</p>
<p>11 (159.5)</p></td>
<td>See Note 1</td>
<td><p>2363 (34263)</p>
<p>945 (13702)</p></td>
<td><p>4</p>
<p>4</p></td>
<td><p>214</p>
<p>86</p></td>
<td><p>16.5 (239)</p>
<p>16.5 (239)</p></td>
<td><p>1.5</p>
<p>1.5</p></td>
<td>T (TBD)</td>
<td><p>MIL-STD-1522A</p>
<p>SSP 30559C</p></td>
</tr>
<tr class="even">
<td>Bellows for SCL exit</td>
<td><p>&lt;10</p>
<p>(&lt;610)</p></td>
<td><p>1</p>
<p>(14.5)</p></td>
<td><p>AISI 316 L</p>
<p>AISI 316 L</p></td>
<td><p>1.8</p>
<p>300</p></td>
<td><p>11 (159.5)</p>
<p>11 (159.5)</p></td>
<td>See Note 1</td>
<td><p>&gt;44 (&gt;638)</p>
<p>&gt;44 (&gt;638)</p></td>
<td><p>4</p>
<p>4</p></td>
<td><p>&gt;4</p>
<p>&gt;4</p></td>
<td><p>16.5 (239)</p>
<p>16.5 (239)</p></td>
<td><p>1.5</p>
<p>1.5</p></td>
<td>T (TBD)</td>
<td><p>MIL-STD-1522A</p>
<p>SSP 30559C</p></td>
</tr>
<tr class="odd">
<td>SCL External Flexible Line</td>
<td><p>&lt;10</p>
<p>(&lt;610)</p></td>
<td><p>1</p>
<p>(14.5)</p></td>
<td>AISI 316 L</td>
<td>300</td>
<td>11 (159.5)</td>
<td>See Note 1</td>
<td>&gt;44 (&gt;638)</td>
<td>4</td>
<td>&gt;4</td>
<td>16.5 (239)</td>
<td>1.5</td>
<td>T (TBD)</td>
<td><p>MIL-STD-1522A</p>
<p>SSP 30559C</p></td>
</tr>
<tr class="even">
<td>Tube from SCL exit to MV43 and MV17</td>
<td><p>&lt;10</p>
<p>(&lt;610)</p></td>
<td><p>1</p>
<p>(14.5)</p></td>
<td>AISI 316 L</td>
<td>300</td>
<td>10 (145)</td>
<td>See Note 1</td>
<td>&gt;40 (&gt;580)</td>
<td>4</td>
<td>&gt;4</td>
<td>15 (217)</td>
<td>1.5</td>
<td>T (TBD)</td>
<td><p>MIL-STD-1522A</p>
<p>SSP 30559C</p></td>
</tr>
<tr class="odd">
<td>Cold Heat Exchanger (CHX)</td>
<td><p>30</p>
<p>(1830)</p></td>
<td><p>1</p>
<p>(14.5)</p></td>
<td><p>Alum</p>
<p>1050A-O</p>
<p>Alum</p>
<p>1050A-O</p></td>
<td><p>1.8</p>
<p>300</p></td>
<td><p>20 (290)</p>
<p>20 (290)</p></td>
<td>See Note 1</td>
<td><p>&gt;180 (&gt;2610)</p>
<p>57 (826)</p></td>
<td><p>2.5</p>
<p>2.5</p></td>
<td><p>&gt;9</p>
<p>2.85</p></td>
<td><p>30.0 (435)</p>
<p>30.0 (435)</p></td>
<td><p>1.5</p>
<p>1.5</p></td>
<td>T</td>
<td>Hans Bieri Engineering</td>
</tr>
<tr class="even">
<td>Cold Heat Exchanger (CHX) – Small Tube</td>
<td><p>10</p>
<p>(610)</p></td>
<td><p>1</p>
<p>(14.5)</p></td>
<td><p>Alum</p>
<p>1050A-O</p>
<p>Alum</p>
<p>1050A-O</p></td>
<td><p>1.8</p>
<p>300</p></td>
<td><p>20 (290)</p>
<p>20 (290)</p></td>
<td>See Note 1</td>
<td><p>301 (4364)</p>
<p>97 (1406)</p></td>
<td><p>4</p>
<p>4</p></td>
<td><p>15</p>
<p>4.9</p></td>
<td><p>30.0 (435)</p>
<p>30.0 (435)</p></td>
<td><p>1.5</p>
<p>1.5</p></td>
<td>T</td>
<td>Hans Bieri Engineering</td>
</tr>
<tr class="odd">
<td>Cold Heat Exchanger (CHX) – Large Tube</td>
<td><p>20</p>
<p>(1220)</p></td>
<td><p>1</p>
<p>(14.5)</p></td>
<td><p>Alum</p>
<p>1050A-O</p>
<p>Alum</p>
<p>1050A-O</p></td>
<td><p>1.8</p>
<p>300</p></td>
<td><p>20 (290)</p>
<p>20 (290)</p></td>
<td>See Note 1</td>
<td><p>155 (2247)</p>
<p>50 (725)</p></td>
<td><p>2.5</p>
<p>2.5</p></td>
<td><p>7.75</p>
<p>2.5</p></td>
<td><p>30.0 (435)</p>
<p>30.0 (435)</p></td>
<td><p>1.5</p>
<p>1.5</p></td>
<td>T</td>
<td>Hans Bieri Engineering</td>
</tr>
<tr class="even">
<td><p>Radiation</p>
<p>Shield Vent Line</p></td>
<td><p>&lt;10</p>
<p>(&lt;610)</p></td>
<td><p>0.016</p>
<p>(0.23)</p></td>
<td><p>AISI 316 L</p>
<p>AISI 316 L</p></td>
<td><p>1.8</p>
<p>300</p></td>
<td><p>11 (159.5)</p>
<p>11 (159.5)</p></td>
<td>See Note 1</td>
<td><p>909 (13180)</p>
<p>223 (3233)</p></td>
<td><p>4</p>
<p>4</p></td>
<td><p>83</p>
<p>20</p></td>
<td><p>16.5 (239)</p>
<p>16.5 (239)</p></td>
<td><p>1.5</p>
<p>1.5</p></td>
<td><p>A</p>
<p>A</p></td>
<td><p>MIL-STD-1522A</p>
<p>SSP 30559C</p></td>
</tr>
<tr class="odd">
<td>Radiation Screen Exhaust Exit</td>
<td><p>&lt;10</p>
<p>(&lt;610)</p></td>
<td><p>0.016</p>
<p>(0.23)</p></td>
<td><p>AISI 316 L</p>
<p>AISI 316 L</p></td>
<td><p>1.8</p>
<p>300</p></td>
<td><p>10 (145)</p>
<p>10 (145)</p></td>
<td>See Note 1</td>
<td><p>666 (9657)</p>
<p>266 (3857)</p></td>
<td><p>4</p>
<p>4</p></td>
<td><p>66</p>
<p>26</p></td>
<td><p>15 (217)</p>
<p>15 (217)</p></td>
<td><p>1.5</p>
<p>1.5</p></td>
<td><p>A</p>
<p>A</p></td>
<td><p>MIL-STD-1522A</p>
<p>SSP 30559C</p></td>
</tr>
<tr class="even">
<td>Radiation Screen Exhaust T-Adaptor</td>
<td><p>&lt;10</p>
<p>(&lt;610)</p></td>
<td><p>0.016</p>
<p>(0.23)</p></td>
<td><p>AISI 316 L</p>
<p>AISI 316 L</p></td>
<td><p>1.8</p>
<p>300</p></td>
<td><p>10 (145)</p>
<p>10 (145)</p></td>
<td>See Note 1</td>
<td><p>1173 (17008)</p>
<p>469 (6800)</p></td>
<td><p>4</p>
<p>4</p></td>
<td><p>117</p>
<p>46</p></td>
<td><p>15 (217)</p>
<p>15 (217)</p></td>
<td><p>1.5</p>
<p>1.5</p></td>
<td><p>A</p>
<p>A</p></td>
<td><p>MIL-STD-1522A</p>
<p>SSP 30559C</p></td>
</tr>
<tr class="odd">
<td>Tube from Radiation Screen Exhaust to DV15 Valves</td>
<td><p>&lt;10</p>
<p>(&lt;610)</p></td>
<td><p>0.016</p>
<p>(0.23)</p></td>
<td><p>AISI 316 L</p>
<p>AISI 316 L</p></td>
<td><p>1.8</p>
<p>300</p></td>
<td><p>10 (145)</p>
<p>10 (145)</p></td>
<td>See Note 1</td>
<td><p>2363 (34263)</p>
<p>945 (13702)</p></td>
<td><p>4</p>
<p>4</p></td>
<td><p>236</p>
<p>94</p></td>
<td><p>15 (217)</p>
<p>15 (217)</p></td>
<td><p>1.5</p>
<p>1.5</p></td>
<td><p>A</p>
<p>A</p></td>
<td><p>MIL-STD-1522A</p>
<p>SSP 30559C</p></td>
</tr>
<tr class="even">
<td>External Tubing to MV34A&amp;B</td>
<td><p>&lt;10</p>
<p>(&lt;610)</p></td>
<td><p>0.016</p>
<p>(0.23)</p></td>
<td><p>AISI 316 L</p>
<p>AISI 316 L</p></td>
<td><p>1.8</p>
<p>300</p></td>
<td><p>10 (145)</p>
<p>10 (145)</p></td>
<td>See Note 1</td>
<td><p>2363 (34263)</p>
<p>945 (13702)</p></td>
<td><p>4</p>
<p>4</p></td>
<td><p>236</p>
<p>94</p></td>
<td><p>15 (217)</p>
<p>15 (217)</p></td>
<td><p>1.5</p>
<p>1.5</p></td>
<td><p>A</p>
<p>A</p></td>
<td><p>MIL-STD-1522A</p>
<p>SSP 30559C</p></td>
</tr>
<tr class="odd">
<td>Tube from Porous Plug (PPS) to Squashed pipe</td>
<td><p>&lt;10</p>
<p>(&lt;610)</p></td>
<td><p>0.016</p>
<p>(0.23)</p></td>
<td><p>AISI 316 L</p>
<p>AISI 316 L</p></td>
<td><p>1.8</p>
<p>300</p></td>
<td><p>3 (43.5)</p>
<p>3 (43.5)</p></td>
<td>See Note 1</td>
<td><p>2888 (41876)</p>
<p>1155 (16747)</p></td>
<td><p>4</p>
<p>4</p></td>
<td><p>262</p>
<p>105</p></td>
<td><p>16.5 (239.5)</p>
<p>16.5 (239.5)</p></td>
<td><p>1.5</p>
<p>1.5</p></td>
<td>T (TBD)</td>
<td><p>MIL-STD-1522A</p>
<p>SSP 30559C</p></td>
</tr>
<tr class="even">
<td>Squashed pipe</td>
<td><p>&lt;10</p>
<p>(&lt;610)</p></td>
<td><p>0.016</p>
<p>(0.23)</p></td>
<td><p>AISI 316 L</p>
<p>AISI 316 L</p></td>
<td><p>1.8</p>
<p>300</p></td>
<td><p>11 (159.5)</p>
<p>11 (159.5)</p></td>
<td>See Note 1</td>
<td><p>818 (11861)</p>
<p>327 (4741)</p></td>
<td><p>4</p>
<p>4</p></td>
<td><p>74</p>
<p>29</p></td>
<td><p>16.5 (239.5)</p>
<p>16.5 (239.5)</p></td>
<td><p>1.5</p>
<p>1.5</p></td>
<td>T (TBD)</td>
<td><p>MIL-STD-1522A</p>
<p>SSP 30559C</p></td>
</tr>
<tr class="odd">
<td>Tube from PPS Squashed pipe to 10 mm tube</td>
<td><p>&lt;10</p>
<p>(&lt;610)</p></td>
<td><p>0.016</p>
<p>(0.23)</p></td>
<td><p>AISI 316 L</p>
<p>AISI 316 L</p></td>
<td><p>1.8</p>
<p>300</p></td>
<td><p>11 (159.5)</p>
<p>11 (159.5)</p></td>
<td>See Note 1</td>
<td><p>2363 (34263)</p>
<p>945 (13702)</p></td>
<td><p>4</p>
<p>4</p></td>
<td><p>214</p>
<p>86</p></td>
<td><p>16.5 (239.5)</p>
<p>16.5 (239.5)</p></td>
<td><p>1.5</p>
<p>1.5</p></td>
<td>T (TBD)</td>
<td><p>MIL-STD-1522A</p>
<p>SSP 30559C</p></td>
</tr>
<tr class="even">
<td>10 mm tube to RV02</td>
<td><p>&lt;10</p>
<p>(&lt;610)</p></td>
<td><p>0.016</p>
<p>(0.23)</p></td>
<td><p>AISI 316 L</p>
<p>AISI 316 L</p></td>
<td><p>1.8</p>
<p>300</p></td>
<td><p>11 (159.5)</p>
<p>11 (159.5)</p></td>
<td>See Note 1</td>
<td><p>1368 (19836)</p>
<p>547 (7931)</p></td>
<td><p>4</p>
<p>4</p></td>
<td><p>124</p>
<p>49</p></td>
<td><p>16.5 (239.5)</p>
<p>16.5 (239.5)</p></td>
<td><p>1.5</p>
<p>1.5</p></td>
<td>T (TBD)</td>
<td><p>MIL-STD-1522A</p>
<p>SSP 30559C</p></td>
</tr>
<tr class="odd">
<td>Tube from T-Junction to RV02</td>
<td><p>&lt;10</p>
<p>(&lt;610)</p></td>
<td><p>0.016</p>
<p>(0.23)</p></td>
<td><p>AISI 316 L</p>
<p>AISI 316 L</p></td>
<td><p>1.8</p>
<p>300</p></td>
<td><p>11 (159.5)</p>
<p>11 (159.5)</p></td>
<td>See Note 1</td>
<td><p>1368 (19836)</p>
<p>547 (7931)</p></td>
<td><p>4</p>
<p>4</p></td>
<td><p>124</p>
<p>49</p></td>
<td><p>16.5 (239.5)</p>
<p>16.5 (239.5)</p></td>
<td><p>1.5</p>
<p>1.5</p></td>
<td>T (TBD)</td>
<td><p>MIL-STD-1522A</p>
<p>SSP 30559C</p></td>
</tr>
<tr class="even">
<td>Tube from T-Junction to DV05</td>
<td><p>&lt;10</p>
<p>(&lt;610)</p></td>
<td><p>0.016</p>
<p>(0.23)</p></td>
<td><p>AISI 316 L</p>
<p>AISI 316 L</p></td>
<td><p>1.8</p>
<p>300</p></td>
<td><p>11 (159.5)</p>
<p>11 (159.5)</p></td>
<td>See Note 1</td>
<td><p>1368 (19836)</p>
<p>547 (7931)</p></td>
<td><p>4</p>
<p>4</p></td>
<td><p>124</p>
<p>49</p></td>
<td><p>16.5 (239.5)</p>
<p>16.5 (239.5)</p></td>
<td><p>1.5</p>
<p>1.5</p></td>
<td>T (TBD)</td>
<td><p>MIL-STD-1522A</p>
<p>SSP 30559C</p></td>
</tr>
<tr class="odd">
<td>Tube from T-Junction to DV10</td>
<td><p>&lt;10</p>
<p>(&lt;610)</p></td>
<td><p>0.016</p>
<p>(0.23)</p></td>
<td><p>AISI 316 L</p>
<p>AISI 316 L</p></td>
<td><p>1.8</p>
<p>300</p></td>
<td><p>11 (159.5)</p>
<p>11 (159.5)</p></td>
<td>See Note 1</td>
<td><p>1368 (19836)</p>
<p>547 (7931)</p></td>
<td><p>4</p>
<p>4</p></td>
<td><p>124</p>
<p>49</p></td>
<td><p>16.5 (239.5)</p>
<p>16.5 (239.5)</p></td>
<td><p>1.5</p>
<p>1.5</p></td>
<td>T (TBD)</td>
<td><p>MIL-STD-1522A</p>
<p>SSP 30559C</p></td>
</tr>
<tr class="even">
<td>Tube from T-Junction to Radiation Shield loop</td>
<td><p>&lt;10</p>
<p>(&lt;610)</p></td>
<td><p>0.016</p>
<p>(0.23)</p></td>
<td><p>AISI 316 L</p>
<p>AISI 316 L</p></td>
<td><p>1.8</p>
<p>300</p></td>
<td><p>11 (159.5)</p>
<p>11 (159.5)</p></td>
<td>See Note 1</td>
<td><p>1368 (19836)</p>
<p>547 (7931)</p></td>
<td><p>4</p>
<p>4</p></td>
<td><p>124</p>
<p>49</p></td>
<td><p>16.5 (239.5)</p>
<p>16.5 (239.5)</p></td>
<td><p>1.5</p>
<p>1.5</p></td>
<td>T (TBD)</td>
<td><p>MIL-STD-1522A</p>
<p>SSP 30559C</p></td>
</tr>
<tr class="odd">
<td>Tube from DV05 and RV0 2 to Helium Vessel</td>
<td><p>&lt;10</p>
<p>(&lt;610)</p></td>
<td><p>0.016</p>
<p>(0.23)</p></td>
<td><p>AISI 316 L</p>
<p>AISI 316 L</p></td>
<td><p>1.8</p>
<p>300</p></td>
<td><p>11 (159.5)</p>
<p>11 (159.5)</p></td>
<td>See Note 1</td>
<td><p>1083 (15703)</p>
<p>433 (6278)</p></td>
<td><p>4</p>
<p>4</p></td>
<td><p>98</p>
<p>39</p></td>
<td><p>16.5 (239.5)</p>
<p>16.5 (239.5)</p></td>
<td><p>1.5</p>
<p>1.5</p></td>
<td>T (TBD)</td>
<td><p>MIL-STD-1522A</p>
<p>SSP 30559C</p></td>
</tr>
<tr class="even">
<td>Tube from DV10 to VCS1</td>
<td><p>&lt;10</p>
<p>(&lt;610)</p></td>
<td><p>0.016</p>
<p>(0.23)</p></td>
<td><p>AISI 316 L</p>
<p>AISI 316 L</p></td>
<td><p>1.8</p>
<p>300</p></td>
<td><p>11 (159.5)</p>
<p>11 (159.5)</p></td>
<td>See Note 1</td>
<td><p>1368 (19836)</p>
<p>547 (7931)</p></td>
<td><p>4</p>
<p>4</p></td>
<td><p>124</p>
<p>49</p></td>
<td><p>16.5 (239.5)</p>
<p>16.5 (239.5)</p></td>
<td><p>1.5</p>
<p>1.5</p></td>
<td>T (TBD)</td>
<td><p>MIL-STD-1522A</p>
<p>SSP 30559C</p></td>
</tr>
<tr class="odd">
<td>Tube for VCS1</td>
<td><p>&lt;10</p>
<p>(&lt;610)</p></td>
<td><p>0.016</p>
<p>(0.23)</p></td>
<td><p>AISI 316 L</p>
<p>AISI 316 L</p></td>
<td><p>1.8</p>
<p>300</p></td>
<td><p>11 (159.5)</p>
<p>11 (159.5)</p></td>
<td>See Note 1</td>
<td><p>1130 (16385)</p>
<p>452 (6554)</p></td>
<td><p>4</p>
<p>4</p></td>
<td><p>87</p>
<p>35</p></td>
<td><p>16.5 (239.5)</p>
<p>16.5 (239.5)</p></td>
<td><p>1.5</p>
<p>1.5</p></td>
<td>T (TBD)</td>
<td><p>MIL-STD-1522A</p>
<p>SSP 30559C</p></td>
</tr>
<tr class="even">
<td>Tube for VCS2</td>
<td><p>&lt;10</p>
<p>(&lt;610)</p></td>
<td><p>0.016</p>
<p>(0.23)</p></td>
<td><p>AISI 316 L</p>
<p>AISI 316 L</p></td>
<td><p>1.8</p>
<p>300</p></td>
<td><p>11 (159.5)</p>
<p>11 (159.5)</p></td>
<td>See Note 1</td>
<td><p>963 (13963)</p>
<p>385 (5582)</p></td>
<td><p>4</p>
<p>4</p></td>
<td><p>124</p>
<p>49</p></td>
<td><p>16.5 (239.5)</p>
<p>16.5 (239.5)</p></td>
<td><p>1.5</p>
<p>1.5</p></td>
<td>T (TBD)</td>
<td><p>MIL-STD-1522A</p>
<p>SSP 30559C</p></td>
</tr>
<tr class="odd">
<td>Tube for VCS3</td>
<td><p>&lt;10</p>
<p>(&lt;610)</p></td>
<td><p>0.016</p>
<p>(0.23)</p></td>
<td><p>AISI 316 L</p>
<p>AISI 316 L</p></td>
<td><p>1.8</p>
<p>300</p></td>
<td><p>11 (159.5)</p>
<p>11 (159.5)</p></td>
<td>See Note 1</td>
<td><p>838 (12151)</p>
<p>335 (4857)</p></td>
<td><p>4</p>
<p>4</p></td>
<td><p>76</p>
<p>30</p></td>
<td><p>16.5 (239.5)</p>
<p>16.5 (239.5)</p></td>
<td><p>1.5</p>
<p>1.5</p></td>
<td>T (TBD)</td>
<td><p>MIL-STD-1522A</p>
<p>SSP 30559C</p></td>
</tr>
<tr class="even">
<td>Tube for VCS4</td>
<td><p>&lt;10</p>
<p>(&lt;610)</p></td>
<td><p>0.016</p>
<p>(0.23)</p></td>
<td><p>AISI 316 L</p>
<p>AISI 316 L</p></td>
<td><p>1.8</p>
<p>300</p></td>
<td><p>11 (159.5)</p>
<p>11 (159.5)</p></td>
<td>See Note 1</td>
<td><p>509 (7380)</p>
<p>203 (2943)</p></td>
<td><p>4</p>
<p>4</p></td>
<td><p>46</p>
<p>18</p></td>
<td><p>16.5 (239.5)</p>
<p>16.5 (239.5)</p></td>
<td><p>1.5</p>
<p>1.5</p></td>
<td>T (TBD)</td>
<td><p>MIL-STD-1522A</p>
<p>SSP 30559C</p></td>
</tr>
<tr class="odd">
<td>Exit tube from VCS for Current Lead Cooling</td>
<td><p>&lt;10</p>
<p>(&lt;610)</p></td>
<td><p>0.016</p>
<p>(0.23)</p></td>
<td><p>AISI 316 L</p>
<p>AISI 316 L</p></td>
<td><p>1.8</p>
<p>300</p></td>
<td><p>11 (159.5)</p>
<p>11 (159.5)</p></td>
<td>See Note 1</td>
<td><p>426 (6177)</p>
<p>170 (2465)</p></td>
<td><p>4</p>
<p>4</p></td>
<td><p>38</p>
<p>15</p></td>
<td><p>16.5 (239.5)</p>
<p>16.5 (239.5)</p></td>
<td><p>1.5</p>
<p>1.5</p></td>
<td>T (TBD)</td>
<td><p>MIL-STD-1522A</p>
<p>SSP 30559C</p></td>
</tr>
<tr class="even">
<td>Tube from DV10 to Junction with DV03</td>
<td><p>&lt;10</p>
<p>(&lt;610)</p></td>
<td>1 (14.5)</td>
<td><p>AISI 316 L</p>
<p>AISI 316 L</p></td>
<td><p>1.8</p>
<p>300</p></td>
<td><p>11 (159.5)</p>
<p>11 (159.5)</p></td>
<td>See Note 1</td>
<td><p>1368 (19836)</p>
<p>547 (7931)</p></td>
<td><p>4</p>
<p>4</p></td>
<td><p>124</p>
<p>49</p></td>
<td><p>16.5 (239.5)</p>
<p>16.5 (239.5)</p></td>
<td><p>1.5</p>
<p>1.5</p></td>
<td>T (TBD)</td>
<td><p>MIL-STD-1522A</p>
<p>SSP 30559C</p></td>
</tr>
<tr class="odd">
<td>Helium Fill Line</td>
<td><p>&lt;10</p>
<p>(&lt;610)</p></td>
<td>1 (14.5)</td>
<td><p>AISI 316 L</p>
<p>AISI 316 L</p></td>
<td><p>1.8</p>
<p>300</p></td>
<td><p>11 (159.5)</p>
<p>11 (159.5)</p></td>
<td>See Note 1</td>
<td><p>1579 (22895)</p>
<p>505 (7322)</p></td>
<td><p>4</p>
<p>4</p></td>
<td><p>144</p>
<p>46</p></td>
<td><p>16.5 (239.5)</p>
<p>16.5 (239.5)</p></td>
<td><p>1.5</p>
<p>1.5</p></td>
<td><p>A</p>
<p>A</p></td>
<td><p>MIL-STD-1522A</p>
<p>SSP 30559C</p></td>
</tr>
<tr class="even">
<td>Liquid Helium Fill Port</td>
<td><p>&lt;10</p>
<p>(&lt;610)</p></td>
<td>1 (14.5)</td>
<td><p>AISI 304</p>
<p>AISI 304</p></td>
<td><p>1.8</p>
<p>300</p></td>
<td><p>11 (159.5)</p>
<p>10 (145)</p></td>
<td>See Note 1</td>
<td><p>142 (2059)</p>
<p>56 (812)</p></td>
<td><p>2.5</p>
<p>2.5</p></td>
<td><p>14</p>
<p>5</p></td>
<td><p>16.5 (239.5)</p>
<p>15 (217)</p></td>
<td><p>1.5</p>
<p>1.5</p></td>
<td>T (TBD)</td>
<td><p>MIL-STD-1522A</p>
<p>SSP 30559C</p></td>
</tr>
<tr class="odd">
<td>Tube from T-Junction to DV03</td>
<td><p>&lt;10</p>
<p>(&lt;610)</p></td>
<td>1 (14.5)</td>
<td><p>AISI 316 L</p>
<p>AISI 316 L</p></td>
<td><p>1.8</p>
<p>300</p></td>
<td><p>11 (159.5)</p>
<p>11 (159.5)</p></td>
<td>See Note 1</td>
<td><p>1368 (19836)</p>
<p>547 (7931)</p></td>
<td><p>4</p>
<p>4</p></td>
<td><p>124</p>
<p>49</p></td>
<td><p>16.5 (239.5)</p>
<p>16.5 (239.5)</p></td>
<td><p>1.5</p>
<p>1.5</p></td>
<td>T (TBD)</td>
<td><p>MIL-STD-1522A</p>
<p>SSP 30559C</p></td>
</tr>
<tr class="even">
<td>Tube from T-Junction to Fill Port</td>
<td><p>&lt;10</p>
<p>(&lt;610)</p></td>
<td>1 (14.5)</td>
<td><p>AISI 316 L</p>
<p>AISI 316 L</p></td>
<td><p>1.8</p>
<p>300</p></td>
<td><p>11 (159.5)</p>
<p>11 (159.5)</p></td>
<td>See Note 1</td>
<td><p>1368 (19836)</p>
<p>547 (7931)</p></td>
<td><p>4</p>
<p>4</p></td>
<td><p>124</p>
<p>49</p></td>
<td><p>16.5 (239.5)</p>
<p>16.5 (239.5)</p></td>
<td><p>1.5</p>
<p>1.5</p></td>
<td>T (TBD)</td>
<td><p>MIL-STD-1522A</p>
<p>SSP 30559C</p></td>
</tr>
<tr class="odd">
<td>Flexible Line for Fill Port</td>
<td><p>&lt;10</p>
<p>(&lt;610)</p></td>
<td>1 (14.5)</td>
<td><p>AISI 316 L</p>
<p>AISI 316 L</p></td>
<td><p>1.8</p>
<p>300</p></td>
<td><p>11 (159.5)</p>
<p>11 (159.5)</p></td>
<td>See Note 1</td>
<td><p>&gt;44 (&gt;638)</p>
<p>&gt;44 (&gt;638)</p></td>
<td><p>4</p>
<p>4</p></td>
<td><p>&gt;4</p>
<p>&gt;4</p></td>
<td><p>16.5 (239.5)</p>
<p>16.5 (239.5)</p></td>
<td><p>1.5</p>
<p>1.5</p></td>
<td>T (TBD)</td>
<td><p>MIL-STD-1522A</p>
<p>SSP 30559C</p></td>
</tr>
<tr class="even">
<td>Tube from DV03 to Helium Vessel Feedthrough</td>
<td><p>&lt;10</p>
<p>(&lt;610)</p></td>
<td>1 (14.5)</td>
<td><p>AISI 316 L</p>
<p>AISI 316 L</p></td>
<td><p>1.8</p>
<p>300</p></td>
<td><p>11 (159.5)</p>
<p>11 (159.5)</p></td>
<td>See Note 1</td>
<td><p>1083 (15703)</p>
<p>433 (6278)</p></td>
<td><p>4</p>
<p>4</p></td>
<td><p>98</p>
<p>39</p></td>
<td><p>16.5 (239.5)</p>
<p>16.5 (239.5)</p></td>
<td><p>1.5</p>
<p>1.5</p></td>
<td>T (TBD)</td>
<td><p>MIL-STD-1522A</p>
<p>SSP 30559C</p></td>
</tr>
<tr class="odd">
<td>Tube from DV12 to Helium Vessel Feedthrough</td>
<td><p>&lt;10</p>
<p>(&lt;610)</p></td>
<td>1 (14.5)</td>
<td><p>AISI 316 L</p>
<p>AISI 316 L</p></td>
<td><p>1.8</p>
<p>300</p></td>
<td><p>11 (159.5)</p>
<p>11 (159.5)</p></td>
<td>See Note 1</td>
<td><p>896 (12992)</p>
<p>358 (5191)</p></td>
<td><p>4</p>
<p>4</p></td>
<td><p>81</p>
<p>32</p></td>
<td><p>16.5 (239.5)</p>
<p>16.5 (239.5)</p></td>
<td><p>1.5</p>
<p>1.5</p></td>
<td>T (TBD)</td>
<td><p>MIL-STD-1522A</p>
<p>SSP 30559C</p></td>
</tr>
<tr class="even">
<td>First Tube From DV12 to Fill Port</td>
<td><p>&lt;10</p>
<p>(&lt;610)</p></td>
<td>1 (14.5)</td>
<td><p>AISI 316 L</p>
<p>AISI 316 L</p></td>
<td><p>1.8</p>
<p>300</p></td>
<td><p>11 (159.5)</p>
<p>11 (159.5)</p></td>
<td>See Note 1</td>
<td><p>896 (12992)</p>
<p>358 (5191)</p></td>
<td><p>4</p>
<p>4</p></td>
<td><p>81</p>
<p>32</p></td>
<td><p>16.5 (239.5)</p>
<p>16.5 (239.5)</p></td>
<td><p>1.5</p>
<p>1.5</p></td>
<td>T (TBD)</td>
<td><p>MIL-STD-1522A</p>
<p>SSP 30559C</p></td>
</tr>
<tr class="odd">
<td>Second Tube From DV12 to Fill Port</td>
<td><p>&lt;10</p>
<p>(&lt;610)</p></td>
<td>1 (14.5)</td>
<td><p>AISI 316 L</p>
<p>AISI 316 L</p></td>
<td><p>1.8</p>
<p>300</p></td>
<td><p>11 (159.5)</p>
<p>11 (159.5)</p></td>
<td>See Note 1</td>
<td><p>666 (9657)</p>
<p>266 (3857)</p></td>
<td><p>4</p>
<p>4</p></td>
<td><p>60</p>
<p>24</p></td>
<td><p>16.5 (239.5)</p>
<p>16.5 (239.5)</p></td>
<td><p>1.5</p>
<p>1.5</p></td>
<td>T (TBD)</td>
<td><p>MIL-STD-1522A</p>
<p>SSP 30559C</p></td>
</tr>
<tr class="even">
<td>Bellows from DV12 to Fill Port</td>
<td><p>&lt;10</p>
<p>(&lt;610)</p></td>
<td>1 (14.5)</td>
<td><p>AISI 316 L</p>
<p>AISI 316 L</p></td>
<td><p>1.8</p>
<p>300</p></td>
<td><p>11 (159.5)</p>
<p>11 (159.5)</p></td>
<td>See Note 1</td>
<td><p>&gt;44 (&gt;638)</p>
<p>&gt;44 (&gt;638)</p></td>
<td><p>4</p>
<p>4</p></td>
<td><p>&gt;4</p>
<p>&gt;4</p></td>
<td><p>16.5 (239.5)</p>
<p>16.5 (239.5)</p></td>
<td><p>1.5</p>
<p>1.5</p></td>
<td>T (TBD)</td>
<td><p>MIL-STD-1522A</p>
<p>SSP 30559C</p></td>
</tr>
<tr class="odd">
<td>Helium Vent Line</td>
<td><p>&lt;10</p>
<p>(&lt;610)</p></td>
<td>1 (14.5)</td>
<td><p>AISI 316 L</p>
<p>AISI 316 L</p></td>
<td><p>1.8</p>
<p>300</p></td>
<td><p>11 (159.5)</p>
<p>11 (159.5)</p></td>
<td>See Note 1</td>
<td><p>769 (11150)</p>
<p>246 (3567)</p></td>
<td><p>4</p>
<p>4</p></td>
<td><p>70</p>
<p>22</p></td>
<td><p>16.5 (239.5)</p>
<p>16.5 (239.5)</p></td>
<td><p>1.5</p>
<p>1.5</p></td>
<td><p>A</p>
<p>A</p></td>
<td><p>MIL-STD-1522A</p>
<p>SSP 30559C</p></td>
</tr>
<tr class="even">
<td><p>Helium vessel Emergency</p>
<p>Vent Line</p></td>
<td><p>&lt;10</p>
<p>(&lt;610)</p></td>
<td>-1 (-14.5)</td>
<td><p>AISI 316 L</p>
<p>AISI 316 L</p>
<p>AISI 316 L</p>
<p>AISI 316 L</p>
<p>Epoxy-Gl</p>
<p>Epoxy-Gl</p></td>
<td><p>1.8</p>
<p>300</p>
<p>1.8</p>
<p>300</p>
<p>1.8</p>
<p>300</p></td>
<td><p>3 (43.5)</p>
<p>3 (43.5)</p>
<p>3 (43.5)</p>
<p>3 (43.5)</p>
<p>3 (43.5)</p>
<p>3 (43.5)</p></td>
<td>See Note 1</td>
<td><p>195 (2827)</p>
<p>62 (899)</p>
<p>379 (5495)</p>
<p>122 (1769)</p>
<p>586 (8497)</p>
<p>489 (7090)</p></td>
<td><p>2.5</p>
<p>2.5</p>
<p>2.5</p>
<p>2.5</p>
<p>2.5</p>
<p>2.5</p></td>
<td><p>65.0</p>
<p>20.9</p>
<p>127</p>
<p>40</p>
<p>196</p>
<p>163</p></td>
<td><p>4.5 (65.2)</p>
<p>4.5 (65.2)</p>
<p>4.5 (65.2)</p>
<p>4.5 (65.2)</p>
<p>4.5 (65.2)</p>
<p>4.5 (65.2)</p></td>
<td><p>1.5</p>
<p>1.5</p>
<p>1.5</p>
<p>1.5</p>
<p>1.5</p>
<p>1.5</p></td>
<td><p>A</p>
<p>A</p>
<p>A</p>
<p>A</p>
<p>A</p>
<p>A</p></td>
<td><p>NSTS 1700.7B</p>
<p>ISS addendum</p></td>
</tr>
<tr class="odd">
<td>Tube from TMP01 to DV06A&amp;B</td>
<td><p>&lt;10</p>
<p>(&lt;610)</p></td>
<td>0.2 (2.9)</td>
<td><p>AISI 316 L</p>
<p>AISI 316 L</p></td>
<td><p>1.8</p>
<p>300</p></td>
<td><p>3 (43.5)</p>
<p>3 (43.5)</p></td>
<td>See Note 1</td>
<td><p>1368 (19836)</p>
<p>547 (7931)</p></td>
<td><p>4</p>
<p>4</p></td>
<td><p>456</p>
<p>183</p></td>
<td><p>16.5 (239.5)</p>
<p>16.5 (239.5)</p></td>
<td><p>1.5</p>
<p>1.5</p></td>
<td><p>A</p>
<p>A</p></td>
<td><p>MIL-STD-1522A</p>
<p>SSP 30559C</p></td>
</tr>
<tr class="even">
<td>Tube from DV06A&amp;B to current lead bellows</td>
<td><p>&lt;10</p>
<p>(&lt;610)</p></td>
<td>0.2 (2.9)</td>
<td><p>AISI 316 L</p>
<p>AISI 316 L</p></td>
<td><p>1.8</p>
<p>300</p></td>
<td><p>11 (159.5)</p>
<p>11 (159.5)</p></td>
<td>See Note 1</td>
<td><p>1368 (19836)</p>
<p>547 (7931)</p></td>
<td><p>4</p>
<p>4</p></td>
<td><p>124</p>
<p>50</p></td>
<td><p>16.5 (239.5)</p>
<p>16.5 (239.5)</p></td>
<td><p>1.5</p>
<p>1.5</p></td>
<td><p>A</p>
<p>A</p></td>
<td><p>MIL-STD-1522A</p>
<p>SSP 30559C</p></td>
</tr>
<tr class="odd">
<td>Flexible Bellows on Current Leads x 7</td>
<td><p>&lt;10</p>
<p>(&lt;610)</p></td>
<td>0.2 (2.9)</td>
<td><p>AISI 316 L</p>
<p>AISI 316 L</p></td>
<td><p>1.8</p>
<p>300</p></td>
<td><p>11 (159.5)</p>
<p>11 (159.5)</p></td>
<td>See Note 1</td>
<td><p>&gt;44 (&gt;638)</p>
<p>&gt;44 (&gt;638)</p></td>
<td><p>4</p>
<p>4</p></td>
<td><p>&gt;4</p>
<p>&gt;4</p></td>
<td><p>16.5 (239.5)</p>
<p>16.5 (239.5)</p></td>
<td><p>1.5</p>
<p>1.5</p></td>
<td>T (TBD)</td>
<td><p>MIL-STD-1522A</p>
<p>SSP 30559C</p></td>
</tr>
<tr class="even">
<td>Double Ceramic Isolator</td>
<td><p>&lt;10</p>
<p>(&lt;610)</p></td>
<td>0.2 (2.9)</td>
<td><p>NILO 42</p>
<p>NILO 42</p></td>
<td><p>1.8</p>
<p>300</p></td>
<td><p>11 (159.5)</p>
<p>11 (159.5)</p></td>
<td>See Note 1</td>
<td><p>&gt;44 (&gt;638)</p>
<p>419 (6075)</p></td>
<td><p>4</p>
<p>4</p></td>
<td><p>&gt;4</p>
<p>&gt;4</p></td>
<td><p>16.5 (239.5)</p>
<p>16.5 (239.5)</p></td>
<td><p>1.5</p>
<p>1.5</p></td>
<td>T (TBD)</td>
<td><p>MIL-STD-1522A</p>
<p>SSP 30559C</p></td>
</tr>
<tr class="odd">
<td>Ceramic Current Lead Feedthrough</td>
<td><p>&lt;10</p>
<p>(&lt;610)</p></td>
<td>0.2 (2.9)</td>
<td><p>NILO 42</p>
<p>NILO 42</p></td>
<td><p>1.8</p>
<p>300</p></td>
<td><p>3 (159.5)</p>
<p>3 (159.5)</p></td>
<td>See Note 1</td>
<td><p>&gt;12 (&gt;174)</p>
<p>&gt;12 (&gt;174)</p></td>
<td><p>4</p>
<p>4</p></td>
<td><p>&gt;4</p>
<p>&gt;4</p></td>
<td><p>3.3 (47.8)</p>
<p>3.3 (47.8)</p></td>
<td><p>1.1</p>
<p>See Note 12</p></td>
<td>T</td>
<td><p>Type Test done at 1.5 MDP – SCL Doc. 2886 He vessel feed.doc</p>
<p>Proof Test at Bieri Engineering Report No. 450-0</p></td>
</tr>
<tr class="even">
<td>Current Leads Aluminum Extrusion</td>
<td><p>&lt;10</p>
<p>(&lt;610)</p></td>
<td>0.2 (2.9)</td>
<td>Al1050A-0</td>
<td><p>1.8</p>
<p>300</p></td>
<td><p>11 (159.5)</p>
<p>11 (159.5)</p></td>
<td>See Note 1</td>
<td><p>770 (11165)</p>
<p>248 (3451)</p></td>
<td><p>4</p>
<p>4</p></td>
<td><p>68</p>
<p>22</p></td>
<td><p>16.5 (239.5)</p>
<p>16.5 (239.5)</p></td>
<td><p>1.5</p>
<p>1.5</p></td>
<td>T (TBD)</td>
<td><p>MIL-STD-1522A</p>
<p>SSP 30559C</p></td>
</tr>
<tr class="odd">
<td>Current Lead Tubing</td>
<td><p>&lt;10</p>
<p>(&lt;610)</p></td>
<td>0.2 (2.9)</td>
<td>AISI 316 L</td>
<td><p>1.8</p>
<p>300</p></td>
<td><p>11 (159.5)</p>
<p>11 (159.5)</p></td>
<td>See Note 1</td>
<td><p>1368 (19836)</p>
<p>547 (7931)</p></td>
<td><p>4</p>
<p>4</p></td>
<td><p>124</p>
<p>50</p></td>
<td><p>16.5 (239.5)</p>
<p>16.5 (239.5)</p></td>
<td><p>1.5</p>
<p>1.5</p></td>
<td>T (TBD)</td>
<td><p>MIL-STD-1522A</p>
<p>SSP 30559C</p></td>
</tr>
<tr class="even">
<td>Current Lead Tubing Adaptor 10 to 9.5 mm (0.5 mm wall)</td>
<td><p>&lt;10</p>
<p>(&lt;610)</p></td>
<td>0.2 (2.9)</td>
<td>AISI 316 L</td>
<td><p>1.8</p>
<p>300</p></td>
<td><p>11 (159.5)</p>
<p>11 (159.5)</p></td>
<td>See Note 1</td>
<td><p>1368 (19836)</p>
<p>547 (7931)</p></td>
<td><p>4</p>
<p>4</p></td>
<td><p>124</p>
<p>50</p></td>
<td><p>16.5 (239.5)</p>
<p>16.5 (239.5)</p></td>
<td><p>1.5</p>
<p>1.5</p></td>
<td>T (TBD)</td>
<td><p>MIL-STD-1522A</p>
<p>SSP 30559C</p></td>
</tr>
<tr class="odd">
<td>Radiation screen pipe from current leads</td>
<td><p>&lt;10</p>
<p>(&lt;610)</p></td>
<td>0.2 (2.9)</td>
<td>AISI 304</td>
<td><p>1.8</p>
<p>300</p></td>
<td><p>11 (159.5)</p>
<p>11 (159.5)</p></td>
<td>See Note 1</td>
<td><p>1444 (20938)</p>
<p>578 (8381)</p></td>
<td><p>4</p>
<p>4</p></td>
<td><p>131</p>
<p>52</p></td>
<td><p>16.5 (239.5)</p>
<p>16.5 (239.5)</p></td>
<td><p>1.5</p>
<p>1.5</p></td>
<td>T (TBD)</td>
<td><p>MIL-STD-1522A</p>
<p>SSP 30559C</p></td>
</tr>
<tr class="even">
<td>Current Lead Fabrication</td>
<td><p>&lt;10</p>
<p>(&lt;610)</p></td>
<td>0.2 (2.9)</td>
<td>Al1050A-0</td>
<td><p>1.8</p>
<p>300</p></td>
<td><p>11 (159.5)</p>
<p>11 (159.5)</p></td>
<td>See Note 1</td>
<td><p>528 (7656)</p>
<p>170 (2465)</p></td>
<td><p>4</p>
<p>4</p></td>
<td><p>48</p>
<p>15</p></td>
<td><p>16.5 (239.5)</p>
<p>16.5 (239.5)</p></td>
<td><p>1.5</p>
<p>1.5</p></td>
<td>T (TBD)</td>
<td><p>MIL-STD-1522A</p>
<p>SSP 30559C</p></td>
</tr>
<tr class="odd">
<td>Current Lead 90 Degree Elbow</td>
<td><p>&lt;10</p>
<p>(&lt;610)</p></td>
<td>0.2 (2.9)</td>
<td>Al1050A-0</td>
<td><p>1.8</p>
<p>300</p></td>
<td><p>11 (159.5)</p>
<p>11 (159.5)</p></td>
<td>See Note 1</td>
<td><p>528 (7656)</p>
<p>170 (2465)</p></td>
<td><p>4</p>
<p>4</p></td>
<td><p>48</p>
<p>15</p></td>
<td><p>16.5 (239.5)</p>
<p>16.5 (239.5)</p></td>
<td><p>1.5</p>
<p>1.5</p></td>
<td>T (TBD)</td>
<td><p>MIL-STD-1522A</p>
<p>SSP 30559C</p></td>
</tr>
<tr class="even">
<td>Current Lead Exit Dual Ceramic SCD2064</td>
<td><p>&lt;10</p>
<p>(&lt;610)</p></td>
<td>0.2 (2.9)</td>
<td>NILO 42</td>
<td><p>1.8</p>
<p>300</p></td>
<td><p>11 (159.5)</p>
<p>11 (159.5)</p></td>
<td>See Note 1</td>
<td><p>&gt;200 (&gt;2900)</p>
<p>200 (2900)</p></td>
<td><p>4</p>
<p>4</p></td>
<td><p>&gt;18</p>
<p>18</p></td>
<td><p>16.5 (239.5)</p>
<p>16.5 (239.5)</p></td>
<td><p>1.5</p>
<p>1.5</p></td>
<td>T (TBD)</td>
<td></td>
</tr>
<tr class="odd">
<td>Current Lead Exit Bellows</td>
<td><p>&lt;10</p>
<p>(&lt;610)</p></td>
<td>0.2 (2.9)</td>
<td>AISI 316 L</td>
<td><p>1.8</p>
<p>300</p></td>
<td><p>11 (159.5)</p>
<p>11 (159.5)</p></td>
<td>See Note 1</td>
<td><p>&gt;44 (&gt;638)</p>
<p>&gt;44 (&gt;638)</p></td>
<td><p>4</p>
<p>4</p></td>
<td><p>&gt;4</p>
<p>&gt;4</p></td>
<td><p>16.5 (239.5)</p>
<p>16.5 (239.5)</p></td>
<td><p>1.5</p>
<p>1.5</p></td>
<td>T (TBD)</td>
<td><p>MIL-STD-1522A</p>
<p>SSP 30559C</p></td>
</tr>
<tr class="even">
<td>Current Lead Disconnect Helium Feed Tubing</td>
<td><p>&lt;10</p>
<p>(&lt;610)</p></td>
<td>6 (87)</td>
<td>AISI 316 L</td>
<td><p>1.8</p>
<p>300</p></td>
<td><p>11 (159.5)</p>
<p>11 (159.5)</p></td>
<td>See Note 1</td>
<td><p>5200 (75400)</p>
<p>2080 (30160)</p></td>
<td><p>4</p>
<p>4</p></td>
<td><p>472</p>
<p>189</p></td>
<td><p>16.5 (239.5)</p>
<p>16.5 (239.5)</p></td>
<td><p>1.5</p>
<p>1.5</p></td>
<td>T (TBD)</td>
<td><p>MIL-STD-1522A</p>
<p>SSP 30559C</p></td>
</tr>
<tr class="odd">
<td>Current Lead Line</td>
<td><p>&lt;10</p>
<p>(&lt;610)</p></td>
<td>0.2 (2.9)</td>
<td><p>AISI 316 L</p>
<p>AISI 316 L</p>
<p>Al1050A-0</p>
<p>Al1050A-0</p></td>
<td><p>1.8</p>
<p>300</p>
<p>1.8</p>
<p>300</p></td>
<td><p>11 (159.5)</p>
<p>11 (159.5)</p>
<p>11 (159.5)</p>
<p>11 (159.5)</p></td>
<td>See Note 1</td>
<td><p>1575 (22837)</p>
<p>504 (7308)</p>
<p>466 (6757)</p>
<p>150 (2175)</p></td>
<td><p>4</p>
<p>4</p>
<p>4</p>
<p>4</p></td>
<td><p>143</p>
<p>46</p>
<p>42</p>
<p>13.6</p></td>
<td><p>16.5 (239.5)</p>
<p>16.5 (239.5)</p>
<p>16.5 (239.5)</p>
<p>16.5 (239.5)</p></td>
<td><p>1.5</p>
<p>1.5</p>
<p>1.5</p>
<p>1.5</p></td>
<td>T (TBD)</td>
<td><p>MIL-STD-1522A</p>
<p>SSP 30559C</p></td>
</tr>
<tr class="even">
<td>Current Lead Exit Tubing</td>
<td><p>&lt;10</p>
<p>(&lt;610)</p></td>
<td>0.2 (2.9)</td>
<td>AISI 316 L</td>
<td><p>1.8</p>
<p>300</p></td>
<td><p>10 (145)</p>
<p>10 (145)</p></td>
<td>See Note 1</td>
<td><p>2363 (34263)</p>
<p>945 (13702)</p></td>
<td><p>4</p>
<p>4</p></td>
<td><p>236</p>
<p>94</p></td>
<td><p>15 (217)</p>
<p>15 (217)</p></td>
<td><p>1.5</p>
<p>1.5</p></td>
<td>T (TBD)</td>
<td><p>MIL-STD-1522A</p>
<p>SSP 30559C</p></td>
</tr>
<tr class="odd">
<td><p>Bi-metal on SCL (SCD0905</p>
<p>-15)</p></td>
<td>-</td>
<td>0.016 (0.23)</td>
<td><p>AISI 316 L</p>
<p>5083-H321</p>
<p>(welded)</p>
<p>AISI 316 L</p>
<p>5083-H321</p>
<p>(welded)</p></td>
<td><p>1.8</p>
<p>1.8</p>
<p>300</p>
<p>300</p></td>
<td><p>23(333.5)</p>
<p>23(333.5)</p>
<p>20 (290)</p>
<p>20 (290)</p></td>
<td>See Note 1</td>
<td><p>1020 (14790)</p>
<p>703 (10193)</p>
<p>408 (5916)</p>
<p>588 (8526)</p></td>
<td><p>2.5</p>
<p>2.5</p>
<p>2.5</p>
<p>2.5</p></td>
<td><p>44.3</p>
<p>30.6</p>
<p>16.3</p>
<p>23.5</p></td>
<td><p>34.5(500)</p>
<p>34.5(500)</p>
<p>30.0(435)</p>
<p>30.0(435)</p></td>
<td><p>1.5</p>
<p>1.5</p>
<p>1.5</p>
<p>1.5</p></td>
<td>T (TBD)</td>
<td><p>MIL-STD-1522A</p>
<p>SSP 30559C</p></td>
</tr>
<tr class="even">
<td>BD03 Feedthrough Assembly SCD0905-10</td>
<td>&lt;10 (&lt;610)</td>
<td>0.016 (0.23)</td>
<td><p>AISI 316 L</p>
<p>5083-H321</p>
<p>(welded)</p>
<p>AISI 316 L</p>
<p>5083-H321</p>
<p>(welded)</p></td>
<td><p>1.8</p>
<p>1.8</p>
<p>300</p>
<p>300</p></td>
<td><p>3 (43.5)</p>
<p>3(43.5)</p>
<p>3(43.5)</p>
<p>3(43.5)</p></td>
<td>See Note 1</td>
<td><p>169 (2450)</p>
<p>141 (2044)</p></td>
<td><p>2.5</p>
<p>2.5</p>
<p>2.5</p>
<p>2.5</p></td>
<td><p>56</p>
<p>47</p></td>
<td>3.3 (47.8)</td>
<td><p>1.1</p>
<p>see Note 12</p></td>
<td>T</td>
<td><p>MIL-STD-1522A</p>
<p>SSP 30559C</p>
<p>Proof Test at Bieri Engineering Report No. 450-0</p></td>
</tr>
<tr class="odd">
<td>TMP Feedthroughs SCD0905-49</td>
<td>&lt;10 (&lt;610)</td>
<td>0.016 (0.23)</td>
<td><p>AISI 316 L</p>
<p>5083-H321</p>
<p>(welded)</p>
<p>AISI 316 L</p>
<p>5083-H321</p>
<p>(welded)</p></td>
<td><p>1.8</p>
<p>1.8</p>
<p>300</p>
<p>300</p></td>
<td><p>3 (43.5)</p>
<p>3(43.5)</p>
<p>3(43.5)</p>
<p>3(43.5)</p></td>
<td>See Note 1</td>
<td><p>411 (5959)</p>
<p>343 (4973)</p></td>
<td><p>2.5</p>
<p>2.5</p>
<p>2.5</p>
<p>2.5</p></td>
<td><p>137</p>
<p>114</p></td>
<td>3.3 (47.8)</td>
<td><p>1.1</p>
<p>see Note 12</p></td>
<td>T</td>
<td><p>MIL-STD-1522A</p>
<p>SSP 30559C</p>
<p>Proof Test at Bieri Engineering Report No. 450-0</p></td>
</tr>
<tr class="even">
<td>PPS Feedthrough SCD0905-18</td>
<td>&lt;10 (&lt;610)</td>
<td>0.016 (0.23)</td>
<td><p>AISI 316 L</p>
<p>5083-H321</p>
<p>(welded)</p>
<p>AISI 316 L</p>
<p>5083-H321</p>
<p>(welded)</p></td>
<td><p>1.8</p>
<p>1.8</p>
<p>300</p>
<p>300</p></td>
<td><p>3 (43.5)</p>
<p>3(43.5)</p>
<p>3(43.5)</p>
<p>3(43.5)</p></td>
<td>See Note 1</td>
<td><p>293 (4248)</p>
<p>245 (3552)</p></td>
<td><p>2.5</p>
<p>2.5</p>
<p>2.5</p>
<p>2.5</p></td>
<td><p>98</p>
<p>82</p></td>
<td>3.3 (47.8)</td>
<td><p>1.1</p>
<p>see Note 12</p></td>
<td>T</td>
<td><p>MIL-STD-1522A</p>
<p>SSP 30559C</p>
<p>Proof Test at Bieri Engineering Report No. 450-0</p></td>
</tr>
<tr class="odd">
<td>Electrical Feedthrough SCD0905-31</td>
<td>&lt;10 (&lt;610)</td>
<td>0.016 (0.23)</td>
<td><p>AISI 316 L</p>
<p>5083-H321</p>
<p>(welded)</p>
<p>AISI 316 L</p>
<p>5083-H321</p>
<p>(welded)</p></td>
<td><p>1.8</p>
<p>1.8</p>
<p>300</p>
<p>300</p></td>
<td><p>3 (43.5)</p>
<p>3(43.5)</p>
<p>3(43.5)</p>
<p>3(43.5)</p></td>
<td>See Note 1</td>
<td><p>503 (7293)</p>
<p>420 (6090)</p></td>
<td><p>4</p>
<p>4</p>
<p>4</p>
<p>4</p></td>
<td><p>168</p>
<p>140</p></td>
<td>3.3 (47.8)</td>
<td><p>1.1</p>
<p>see Note 12</p></td>
<td>T</td>
<td><p>MIL-STD-1522A</p>
<p>SSP 30559C</p>
<p>Proof Test at Bieri Engineering Report No. 450-0</p></td>
</tr>
<tr class="even">
<td>Cool Down Circuit Feedthrough SCD0905-36</td>
<td>&lt;10 (&lt;610)</td>
<td>0.016 (0.23)</td>
<td><p>AISI 316 L</p>
<p>5083-H321</p>
<p>(welded)</p>
<p>AISI 316 L</p>
<p>5083-H321</p>
<p>(welded)</p></td>
<td><p>1.8</p>
<p>1.8</p>
<p>300</p>
<p>300</p></td>
<td><p>3 (43.5)</p>
<p>3(43.5)</p>
<p>3(43.5)</p>
<p>3(43.5)</p></td>
<td>See Note 1</td>
<td><p>880 (12760)</p>
<p>735 (10657)</p></td>
<td><p>4</p>
<p>4</p>
<p>4</p>
<p>4</p></td>
<td><p>293</p>
<p>245</p></td>
<td>3.3 (47.8)</td>
<td><p>1.1</p>
<p>see Note 12</p></td>
<td>T</td>
<td><p>MIL-STD-1522A</p>
<p>SSP 30559C</p>
<p>Proof Test at Bieri Engineering Report No. 450-0</p></td>
</tr>
<tr class="odd">
<td>Fill and Pressure relief Feedthroughs SCD0905-17</td>
<td>&lt;10 (&lt;610)</td>
<td>0.016 (0.23)</td>
<td><p>AISI 316 L</p>
<p>5083-H321</p>
<p>(welded)</p>
<p>AISI 316 L</p>
<p>5083-H321</p>
<p>(welded)</p></td>
<td><p>1.8</p>
<p>1.8</p>
<p>300</p>
<p>300</p></td>
<td><p>3 (43.5)</p>
<p>3(43.5)</p>
<p>3(43.5)</p>
<p>3(43.5)</p></td>
<td>See Note 1</td>
<td><p>939 (13615)</p>
<p>784 (11368)</p></td>
<td><p>4</p>
<p>4</p>
<p>4</p>
<p>4</p></td>
<td><p>313</p>
<p>261</p></td>
<td>3.3 (47.8)</td>
<td><p>1.1</p>
<p>see Note 12</p></td>
<td>T</td>
<td><p>MIL-STD-1522A</p>
<p>SSP 30559C</p>
<p>Proof Test at Bieri Engineering Report No. 450-0</p></td>
</tr>
<tr class="even">
<td>Fill gas return Feedthrough SCD0905-37</td>
<td>&lt;10 (&lt;610)</td>
<td>0.016 (0.23)</td>
<td><p>AISI 316 L</p>
<p>5083-H321</p>
<p>(welded)</p>
<p>AISI 316 L</p>
<p>5083-H321</p>
<p>(welded)</p></td>
<td><p>1.8</p>
<p>1.8</p>
<p>300</p>
<p>300</p></td>
<td><p>3 (43.5)</p>
<p>3(43.5)</p>
<p>3(43.5)</p>
<p>3(43.5)</p></td>
<td>See Note 1</td>
<td><p>704 (10208)</p>
<p>588 (8526)</p></td>
<td><p>4</p>
<p>4</p>
<p>4</p>
<p>4</p></td>
<td><p>235</p>
<p>196</p></td>
<td>3.3 (47.8)</td>
<td><p>1.1</p>
<p>see Note 12</p></td>
<td>T (TBD)</td>
<td><p>MIL-STD-1522A</p>
<p>SSP 30559C</p>
<p>Proof Test at Bieri Engineering Report No. 450-0</p></td>
</tr>
<tr class="odd">
<td>Bi-Metal for Current Lead Feedthrough SCD0905-07</td>
<td>&lt;10 (&lt;610)</td>
<td>0.016 (0.23)</td>
<td><p>AISI 316 L</p>
<p>5083-H321</p>
<p>(welded)</p>
<p>AISI 316 L</p>
<p>5083-H321</p>
<p>(welded)</p></td>
<td><p>1.8</p>
<p>1.8</p>
<p>300</p>
<p>300</p></td>
<td><p>3 (43.5)</p>
<p>3(43.5)</p>
<p>3(43.5)</p>
<p>3(43.5)</p></td>
<td>See Note 1</td>
<td><p>632 (9164)</p>
<p>528 (7656)</p></td>
<td><p>2.5</p>
<p>2.5</p>
<p>2.5</p>
<p>2.5</p></td>
<td><p>235</p>
<p>196</p></td>
<td>3.3 (47.8)</td>
<td><p>1.1</p>
<p>see Note 12</p></td>
<td>T (TBD)</td>
<td><p>MIL-STD-1522A</p>
<p>SSP 30559C</p>
<p>Proof Test at Bieri Engineering Report No. 450-0</p></td>
</tr>
<tr class="even">
<td>First Bi-Metal on Current Leads to fabrication SCD1200-11</td>
<td><p>&lt;10</p>
<p>(&lt;610)</p></td>
<td>0.2 (2.9)</td>
<td><p>AISI 316 L</p>
<p>5083-H321</p>
<p>(welded)</p>
<p>AISI 316 L</p>
<p>5083-H321</p>
<p>(welded)</p></td>
<td><p>1.8</p>
<p>300</p></td>
<td><p>11 (159.5)</p>
<p>11 (159.5)</p></td>
<td>See Note 1</td>
<td><p>459 (6655)</p>
<p>383 (5553)</p></td>
<td><p>4</p>
<p>4</p></td>
<td><p>41</p>
<p>35</p></td>
<td><p>16.5 (239.3)</p>
<p>16.5 (239.3)</p></td>
<td><p>1.5</p>
<p>1.5</p></td>
<td>T (TBD)</td>
<td><p>MIL-STD-1522A</p>
<p>SSP 30559C</p></td>
</tr>
<tr class="odd">
<td>Second Bi-Metal on Current Leads to fabrication SCD1200-92</td>
<td><p>&lt;10</p>
<p>(&lt;610)</p></td>
<td>0.2 (2.94)</td>
<td><p>AISI 316 L</p>
<p>5083-H321</p>
<p>(welded)</p>
<p>AISI 316 L</p>
<p>5083-H321</p>
<p>(welded)</p></td>
<td><p>1.8</p>
<p>300</p></td>
<td><p>11 (159.5)</p>
<p>3 (159.5)</p></td>
<td>See Note 1</td>
<td><p>459 (6655)</p>
<p>383 (5553)</p></td>
<td><p>4</p>
<p>4</p></td>
<td><p>41</p>
<p>35</p></td>
<td><p>16.5 (239.3)</p>
<p>16.5 (239.3)</p></td>
<td><p>1.5</p>
<p>1.5</p></td>
<td>T (TBD)</td>
<td><p>MIL-STD-1522A</p>
<p>SSP 30559C</p></td>
</tr>
<tr class="even">
<td><p>Bi-metal on Inst Feed through</p>
<p>(SCD 0905-29</p></td>
<td>-</td>
<td>0.016 (0.23)</td>
<td><p>AISI 316 L</p>
<p>5083-H321</p>
<p>(welded)</p>
<p>AISI 316 L</p>
<p>5083-H321</p>
<p>(welded)</p></td>
<td><p>1.8</p>
<p>1.8</p>
<p>300</p>
<p>300</p></td>
<td><p>3 (43.5)</p>
<p>3 (43.5)</p>
<p>3 (43.5)</p>
<p>3 (43.5)</p></td>
<td>See Note 1</td>
<td><p>666 (9657)</p>
<p>498 (7221)</p>
<p>213 (3088)</p>
<p>333 (4828)</p></td>
<td><p>2.5</p>
<p>2.5</p>
<p>2.5</p>
<p>2.5</p></td>
<td><p>222</p>
<p>166</p>
<p>71.1</p>
<p>111</p></td>
<td>3.3 (47.8)</td>
<td><p>1.1</p>
<p>see Note 12</p></td>
<td>T</td>
<td><p>MIL-STD-1522A</p>
<p>SSP 30559C</p>
<p>Proof Test at Bieri Engineering Report No. 450-0</p></td>
</tr>
<tr class="odd">
<td><p>Bi-metal on DLCM</p>
<p>(SCD 0905</p>
<p>-26)</p></td>
<td>-</td>
<td>0.016 (0.23)</td>
<td><p>AISI 316 L</p>
<p>5083-H321</p>
<p>(welded)</p>
<p>AISI 316 L</p>
<p>5083-H321</p>
<p>(welded)</p></td>
<td><p>1.8</p>
<p>1.8</p>
<p>300</p>
<p>300</p></td>
<td><p>3 (43.5)</p>
<p>3 (43.5)</p>
<p>3 (43.5)</p>
<p>3 (43.5)</p></td>
<td>See Note 1</td>
<td><p>243 (3523)</p>
<p>303 (4393)</p>
<p>78 (1131)</p>
<p>203 (2943)</p></td>
<td><p>2.5</p>
<p>2.5</p>
<p>2.5</p>
<p>2.5</p></td>
<td><p>81.1</p>
<p>101</p>
<p>25.9</p>
<p>67.8</p></td>
<td>3.3 (47.8)</td>
<td><p>1.1</p>
<p>see Note 12</p></td>
<td>T</td>
<td><p>MIL-STD-1522A</p>
<p>SSP 30559C</p>
<p>Proof Test at Bieri Engineering Report No. 450-0</p></td>
</tr>
<tr class="even">
<td><p>Relief Valve</p>
<p>RV02</p></td>
<td><p>&lt;10</p>
<p>(&lt;610)</p></td>
<td>0.016 (0.23)</td>
<td><p>Stainless</p>
<p>Steel and</p>
<p>Vespel</p>
<p>DIN 1.4571</p>
<p>1.4310</p>
<p>Vespel SP-1</p></td>
<td>1.8-300</td>
<td>3 (43.5)</td>
<td>See Note 1</td>
<td>&gt; 25 (&gt;362)</td>
<td>2.5</td>
<td>&gt;8.3</td>
<td>4.5 (65.2)</td>
<td>1.5</td>
<td>-</td>
<td><p>Linde Acceptance data package:</p>
<p>Doc No’s. A-QA 3501/3502</p></td>
</tr>
<tr class="odd">
<td><p>Burst Disc</p>
<p>BD02</p></td>
<td><p>&lt;10</p>
<p>(&lt;610)</p></td>
<td>1 (14.5)</td>
<td>Stainless steel, 316 / 316L</td>
<td><p>300</p>
<p>1.8</p></td>
<td><p>23 (333.5)</p>
<p>See</p>
<p>Note 6</p></td>
<td>-</td>
<td>-</td>
<td>-</td>
<td>-</td>
<td>-</td>
<td>-</td>
<td>T </td>
<td>SCL Testing WI-274</td>
</tr>
<tr class="even">
<td><p>Burst Disc</p>
<p>BD03, BD06A, BD06B</p></td>
<td><p>&lt;10</p>
<p>(&lt;610)</p></td>
<td>0.016 (0.23)</td>
<td>Stainless steel, 316 Nickel 200</td>
<td>300</td>
<td><p>3 (43.5)</p>
<p>See</p>
<p>Note 6</p></td>
<td>-</td>
<td>-</td>
<td>-</td>
<td>-</td>
<td>-</td>
<td>-</td>
<td>T </td>
<td>SCL Testing WI-092</td>
</tr>
<tr class="odd">
<td><p>Pressure</p>
<p>Xducers</p>
<p>P04,P05</p>
<p>Bourdon</p>
<p>Haenni EF01 06</p></td>
<td><p>&lt;10</p>
<p>(&lt;610)</p></td>
<td>0.016 (0.23)</td>
<td><p>15.5 PH steel</p>
<p>Hastelloy C276</p></td>
<td>1.8-300</td>
<td>3 (43.5)</td>
<td>See Note 1</td>
<td>120 (1740)</td>
<td>2.5</td>
<td>16</td>
<td>9 (130.5)</td>
<td>3.0</td>
<td>T</td>
<td>Manufacturers Data Sheet Specifications for max. working
pressure</td>
</tr>
<tr class="even">
<td><p>Pressure transducers P06, P07</p>
<p>AIM Edwards</p></td>
<td><p>&lt;10</p>
<p>(&lt;610)</p></td>
<td>-1 (-14.5)</td>
<td><p>٠Stainless</p>
<p>steel 304,</p>
<p>316, 347</p>
<p>٠Copper</p>
<p>٠Ceramic</p></td>
<td>300</td>
<td>0.8 (11.6)</td>
<td>See Note 1</td>
<td>&gt;10 (&gt;145)</td>
<td>2.5</td>
<td>&gt;2.5</td>
<td>10(145)</td>
<td>1.5</td>
<td>T</td>
<td>Manufacturer data for working pressure</td>
</tr>
<tr class="odd">
<td><p>Thermo</p>
<p>mechanical</p>
<p>pump</p>
<p>TMP01</p></td>
<td><p>&lt;10</p>
<p>(&lt;610)</p></td>
<td>0.2 (2.9)</td>
<td>Stainless steel CRES 300</td>
<td>1.8-300</td>
<td>3 (43.5)</td>
<td>See Note 1</td>
<td>256.2 (3719)</td>
<td>2.5</td>
<td>85.4</td>
<td>4.5 (65.2)</td>
<td>1.5</td>
<td>T</td>
<td>SCL WI 264 – Flight TMP Assembly and Testing</td>
</tr>
<tr class="even">
<td><p>Thermo</p>
<p>mechanical</p>
<p>pump TMP02</p></td>
<td><p>&lt;10</p>
<p>(&lt;610)</p></td>
<td>0.2 (2.9)</td>
<td>Stainless steel CRES 300</td>
<td>1.8-300</td>
<td>3 (43.5)</td>
<td>See Note 1</td>
<td>256.2 (3719)</td>
<td>2.5</td>
<td>85.4</td>
<td>4.5 (65.2)</td>
<td>1.5</td>
<td>T</td>
<td>SCL WI 264 – Flight TMP Assembly and Testing</td>
</tr>
<tr class="odd">
<td><p>Porous Plug</p>
<p>(PPS)</p></td>
<td><p>&lt;10</p>
<p>(&lt;610)</p></td>
<td>0.016 (0.23)</td>
<td>Stainless steel</td>
<td>1.8-300</td>
<td>3 (43.5)</td>
<td>See Note 1</td>
<td>&gt;15 (&gt;217.5)</td>
<td><h1 id="section">2.5</h1></td>
<td>&gt;5</td>
<td>4.5 (65.2)</td>
<td>1.5</td>
<td>-</td>
<td><p>Linde Acceptance data package:</p>
<p>Doc No’s. A-QA 1501/1502</p></td>
</tr>
<tr class="even">
<td><p>Mass</p>
<p>Gauging</p>
<p>(DLCM)</p>
<p>HR01 and</p>
<p>HR02</p></td>
<td><p>&lt;10</p>
<p>(&lt;610)</p></td>
<td>0.016 (0.23)</td>
<td>Stainless steel</td>
<td>1.8-300</td>
<td>3 (43.5)</td>
<td>See Note 1</td>
<td>&gt;15 (&gt;217.5)</td>
<td><h1 id="section-1">2.5</h1></td>
<td>&gt;5</td>
<td>4.5 (65.2)</td>
<td>1.5</td>
<td>-</td>
<td><p>Linde Acceptance data package:</p>
<p>Doc No’s. A-QA 2501/2502</p></td>
</tr>
<tr class="odd">
<td><p>Cryogenic</p>
<p>Valves</p>
<p>DV03, 05, 10, 12</p></td>
<td><p>&lt;10</p>
<p>(&lt;610)</p></td>
<td>0.016 (0.23)</td>
<td>St st 316L/ EN1.4404, 1.4432. 1.4435</td>
<td><p>300</p>
<p>1.8</p></td>
<td><p>11 (159.5)</p>
<p>3 (43.5)</p></td>
<td><p>See Note 1</p>
<p>See Note 1</p></td>
<td><p>&gt;27.5</p>
<p>(&gt;860)</p></td>
<td><h1 id="section-2">2.5</h1></td>
<td>&gt;2.5</td>
<td>16.5 (243)</td>
<td>1.5</td>
<td>T</td>
<td>Weka Qualification documents for DV03, 05, 10, and 12</td>
</tr>
<tr class="even">
<td><p>Cryogenic Valves</p>
<p>DV06a, 06b, 07, 14</p></td>
<td><p>&lt;10</p>
<p>(&lt;610)</p></td>
<td>0.2 (2.94)</td>
<td>St st 316L/ EN1.4404, 1.4432. 1.4435</td>
<td><p>300</p>
<p>1.8</p></td>
<td><p>11 (162)</p>
<p>3 (44)</p></td>
<td><p>See Note 1</p>
<p>See Note 1</p></td>
<td><p>&gt;27.5</p>
<p>(&gt;398.7)</p></td>
<td><h1 id="section-3">2.5</h1></td>
<td>&gt;2.5</td>
<td>16.5 (239.3)</td>
<td>1.5</td>
<td>T</td>
<td>Weka Qualification documents for DV06A &amp; b, 07, and 14</td>
</tr>
<tr class="odd">
<td><p>Cryogenic</p>
<p>Valve</p>
<p>DV02a &amp; b</p></td>
<td><p>&lt;10</p>
<p>(&lt;610)</p></td>
<td>1 (14.5)</td>
<td>St st 316L/ EN1.4404, 1.4432. 1.4435</td>
<td><p>300</p>
<p>1.8</p></td>
<td><p>11 (159.5)</p>
<p>23 (333.5)</p></td>
<td><p>See Note 1</p>
<p>See Note 1</p></td>
<td><p>&gt;58.5</p>
<p>(&gt;848.2)</p></td>
<td><h1 id="section-4">2.5</h1></td>
<td>&gt;2.5</td>
<td>34.5 (500)</td>
<td>1.5</td>
<td>T</td>
<td>Weka Qualification documents for DV02a &amp; b</td>
</tr>
<tr class="even">
<td>Cryogenic Weka valves actuation bellows</td>
<td><p>&lt;10</p>
<p>(&lt;610)</p></td>
<td>6 (87)</td>
<td>St St 316Ti/ EN1.4571</td>
<td><p>300</p>
<p>1.8</p></td>
<td><p>8 (116)</p>
<p>8 (116)</p></td>
<td><p>See Note 1</p>
<p>See Note 1</p></td>
<td><p>&gt;20</p>
<p>(&gt;290)</p></td>
<td><h1 id="section-5">2.5</h1></td>
<td>&gt;2.5</td>
<td>8.8 (127.6)</td>
<td>1.1</td>
<td>T (Weka)</td>
<td>Weka qualification and acceptance tests of cryogenic valves</td>
</tr>
<tr class="odd">
<td><p>Bellows</p>
<p>Actuators in</p>
<p>Current leads</p></td>
<td><p>&lt;10</p>
<p>(&lt;610)</p></td>
<td>6 (87)</td>
<td>Stainless steel 316 L</td>
<td>1.8 - 65</td>
<td>11 (159.5)</td>
<td>See Note 1</td>
<td><p>&gt;27.5</p>
<p>(&gt;398.7)</p></td>
<td><h1 id="section-6">2.5</h1></td>
<td>&gt;2.5</td>
<td><p>&gt;16.5</p>
<p>(&gt;239.3)</p></td>
<td>&gt;1.5</td>
<td><p>T</p>
<p>(TBD)</p></td>
<td></td>
</tr>
<tr class="even">
<td><p>Burst Disc</p>
<p>BD07A</p>
<p>BD07B</p>
<p>BD07C</p></td>
<td><p>&lt;10</p>
<p>(&lt;610)</p></td>
<td>-1 (-14.5)</td>
<td><p>Stainless steel</p>
<p>316L</p>
<p>Nickel 200</p></td>
<td>300</td>
<td><p>1.8 (26.1)</p>
<p>See</p>
<p>Note 6</p></td>
<td>-</td>
<td>-</td>
<td><h1 id="section-7">-</h1></td>
<td>-</td>
<td>-</td>
<td>-</td>
<td><p>T</p>
<p>(TBD)</p></td>
<td></td>
</tr>
<tr class="odd">
<td><p>Burst Disc</p>
<p>BD05A</p>
<p>BD05B</p>
<p>BD13A</p>
<p>BD13B</p></td>
<td><p>&lt;10</p>
<p>(&lt;610)</p></td>
<td>0.016 (0.23)</td>
<td><p>Stainless steel</p>
<p>316L</p>
<p>Nickel 200</p></td>
<td>300</td>
<td><p>11 (159.5)</p>
<p>See</p>
<p>Note 6</p></td>
<td>-</td>
<td>-</td>
<td><h1 id="section-8">-</h1></td>
<td>-</td>
<td>-</td>
<td>-</td>
<td><p>T</p>
<p>(TBD)</p></td>
<td></td>
</tr>
<tr class="even">
<td><p>Burst Disc</p>
<p>BD11A</p>
<p>BD11B</p></td>
<td><p>&lt;10</p>
<p>(&lt;610)</p></td>
<td>1 (14.5)</td>
<td><p>Stainless steel</p>
<p>316L</p>
<p>Nickel 200</p></td>
<td>300</td>
<td><p>11 (159.5)</p>
<p>See</p>
<p>Note 6</p></td>
<td>-</td>
<td>-</td>
<td><h1 id="section-9">-</h1></td>
<td>-</td>
<td>-</td>
<td>-</td>
<td><p>T</p>
<p>(TBD)</p></td>
<td></td>
</tr>
<tr class="odd">
<td><p>Burst Disc</p>
<p>BD12A</p>
<p>BD12B</p>
<p>BD10A</p>
<p>BD10B</p></td>
<td><p>&lt;10</p>
<p>(&lt;610)</p></td>
<td>0.2 (2.9)</td>
<td><p>Stainless steel</p>
<p>316L</p>
<p>Nickel 200</p></td>
<td>300</td>
<td><p>11 (159.5)</p>
<p>See</p>
<p>Note 6</p></td>
<td>-</td>
<td>-</td>
<td><h1 id="section-10">-</h1></td>
<td>-</td>
<td>-</td>
<td>-</td>
<td><p>T</p>
<p>(TBD)</p></td>
<td></td>
</tr>
<tr class="even">
<td><p>Burst Disc</p>
<p>BD17A</p>
<p>BD17B</p></td>
<td><p>&lt;10</p>
<p>(&lt;610)</p></td>
<td>-1 (-14.5)</td>
<td><p>Stainless steel</p>
<p>316L</p>
<p>Nickel 200</p></td>
<td>300</td>
<td><p>11 (159.5)</p>
<p>See</p>
<p>Note 6</p></td>
<td>-</td>
<td>-</td>
<td><h1 id="section-11">-</h1></td>
<td>-</td>
<td>-</td>
<td>-</td>
<td><p>T</p>
<p>(TBD)</p></td>
<td></td>
</tr>
<tr class="odd">
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td><h1 id="section-12"></h1></td>
<td></td>
<td></td>
<td></td>
<td></td>
<td></td>
</tr>
<tr class="even">
<td><p>Warm valves</p>
<p>DV11A-B</p>
<p>DV16A-B</p></td>
<td><p>&lt;10</p>
<p>(&lt;610)</p></td>
<td>0.2 (2.9)</td>
<td>Stainless 316</td>
<td>300</td>
<td>11 (159.5)</td>
<td>See Note 1</td>
<td><p>&gt;27.5</p>
<p>(&gt;398.7)</p></td>
<td><h1 id="section-13">2.5</h1></td>
<td>&gt;2.5</td>
<td>16.5 (239.3)</td>
<td>1.5</td>
<td><p>T</p>
<p>(TBD)</p></td>
<td></td>
</tr>
<tr class="odd">
<td><p>MV17A-B</p>
<p>MV43</p>
<p>MV44 Swagelock valves SS4H</p></td>
<td><p>&lt;10</p>
<p>(&lt;610)</p></td>
<td>1 (14.5)</td>
<td>Stainless 321</td>
<td>300</td>
<td>10 (145)</td>
<td>See Note 1</td>
<td><p>&gt;68</p>
<p>(&gt;986)</p></td>
<td><h1 id="section-14">2.5</h1></td>
<td>&gt;6.8</td>
<td>68 (986)</td>
<td>6.8</td>
<td><p>T</p>
<p>(TBD)</p></td>
<td>Working Pressure of 1000 PSIG states in manufacturers catalog</td>
</tr>
<tr class="even">
<td><p>DV09A-B</p>
<p>DV15A-D</p>
<p>MV34A-B</p></td>
<td><p>&lt;10</p>
<p>(&lt;610)</p></td>
<td>0.016 (0.23)</td>
<td>Stainless 316</td>
<td>300</td>
<td>11 (159.5)</td>
<td>See Note 1</td>
<td><p>&gt;27.5</p>
<p>(&gt;398.7)</p></td>
<td><h1 id="section-15">2.5</h1></td>
<td>&gt;2.5</td>
<td>16.5 (239.3)</td>
<td>1.5</td>
<td><p>T</p>
<p>(TBD)</p></td>
<td></td>
</tr>
<tr class="odd">
<td>MV41</td>
<td>&lt;10 (&lt;610)</td>
<td>0.016</td>
<td>Stainless 316</td>
<td><p>300</p>
<p>1.8</p></td>
<td><p>10 (145)</p>
<p>10 (145)</p></td>
<td>See Note 1</td>
<td><p>&gt;27.5</p>
<p>(&gt;398.7)</p></td>
<td><h1 id="section-16">2.5</h1></td>
<td>&gt;2.5</td>
<td>15 (217.5)</td>
<td>1.5</td>
<td><p>T</p>
<p>(TBD)</p></td>
<td></td>
</tr>
<tr class="even">
<td><p>Moog warm valves</p>
<p>MV33A-B</p></td>
<td><p>&lt;10</p>
<p>(&lt;610)</p></td>
<td>-1 (-14.5)</td>
<td>Stainless 316</td>
<td>300</td>
<td>3 (43.5)</td>
<td>See Note 1</td>
<td><p>110</p>
<p>(1595)</p></td>
<td><h1 id="section-17">2.5</h1></td>
<td>36</td>
<td>66 (957)</td>
<td>22</td>
<td><p>T</p>
<p>(TBD manufacturer)</p></td>
<td>Moog drawing CA25863</td>
</tr>
<tr class="odd">
<td><p>Warm valve</p>
<p>MV30</p></td>
<td><p>&lt;10</p>
<p>(&lt;610)</p></td>
<td>-1 (-14.5)</td>
<td>Stainless 316</td>
<td>300</td>
<td>0.8 (11.6)</td>
<td>See Note 1</td>
<td><p>&gt;4.5</p>
<p>(&gt;65.2)</p></td>
<td><h1 id="section-18">2.5</h1></td>
<td>&gt;2.5</td>
<td>1.2 (17.4)</td>
<td>1.5</td>
<td>T</td>
<td>Manufacturers catalog differential pressure rating</td>
</tr>
<tr class="even">
<td><p>Warm valves</p>
<p>DV20A-D</p></td>
<td><p>&lt;10</p>
<p>(&lt;610)</p></td>
<td>-1 (-14.5)</td>
<td>CRES</td>
<td>300</td>
<td>10 (145)</td>
<td>See Note 1</td>
<td>689.7(10000)</td>
<td><h1 id="section-19">2.5</h1></td>
<td>69.0</td>
<td>413.8(6000)</td>
<td>41.4</td>
<td>-</td>
<td>See Manufacturers Qualification Docs (TBD)</td>
</tr>
<tr class="odd">
<td><p>Warm valves</p>
<p>DV22A-D</p></td>
<td><p>&lt;10</p>
<p>(&lt;610)</p></td>
<td>6 (87)</td>
<td>CRES</td>
<td>300</td>
<td>244(3538)</td>
<td>See Note 1</td>
<td>689.7(10000)</td>
<td><h1 id="section-20">2.5</h1></td>
<td>2.83</td>
<td>413.8(6000)</td>
<td>1.7</td>
<td>-</td>
<td>See Manufacturers Qualification Docs (TBD)</td>
</tr>
<tr class="even">
<td><p>Warm valves</p>
<p>DV21A-D</p>
<p>DV52</p>
<p>DV53</p>
<p>DV55</p>
<p>DV56A-B</p>
<p>DV57</p>
<p>DV60</p>
<p>DV62</p>
<p>DV64</p></td>
<td><p>&lt;10</p>
<p>(&lt;610)</p></td>
<td>6 (87)</td>
<td>PAA GF60, Brass, Spring Steel, Steel, Nitric Rubber, POM,
Aluminium</td>
<td>300</td>
<td>8 (116)</td>
<td>See Note 1</td>
<td><p>&gt;20</p>
<p>(&gt;290)</p></td>
<td><h1 id="section-21">2.5</h1></td>
<td>&gt;2.5</td>
<td>&gt;12 (&gt;174)</td>
<td>&gt;1.5</td>
<td><p>T</p>
<p>(TBD)</p></td>
<td></td>
</tr>
<tr class="odd">
<td><p>Warm Valves</p>
<p>MV40</p></td>
<td><p>&lt;10</p>
<p>(&lt;610)</p></td>
<td><p>Outlet:</p>
<p>6 (87)</p>
<p>Inlet:</p>
<p>200 (2900)</p></td>
<td>Al. Aly., CRES 17-4PH, CRES 300 SER, Nylon</td>
<td>300</td>
<td><p>Outlet:</p>
<p>8 (116)</p>
<p>Inlet:</p>
<p>244(3538))</p></td>
<td>See Note 13</td>
<td><p>&gt;20</p>
<p>(&gt;290)</p>
<p>800(11760)</p></td>
<td><h1 id="section-22">2.5</h1></td>
<td>3.29</td>
<td><p>Outlet:</p>
<p>15.6 (226.2)</p>
<p>See Note 8</p>
<p>Inlet:</p>
<p>480 (6960)</p></td>
<td><p>Inlet:</p>
<p>1.95</p>
<p>Outlet:</p>
<p>1.97</p></td>
<td><p>T</p>
<p>(TBD)</p></td>
<td>Manufacturers data – Marotta</td>
</tr>
<tr class="even">
<td><p>Warm Helium Fill and Drain Port</p>
<p>MV42</p></td>
<td><p>&lt;10</p>
<p>(&lt;610)</p></td>
<td>200 (2900)</td>
<td>6Al4V Titanium</td>
<td>300</td>
<td>244(3538)</td>
<td>See Note 13</td>
<td><p>800</p>
<p>(11600)</p></td>
<td><h1 id="section-23">2.5</h1></td>
<td>3.28</td>
<td>480 (6960)</td>
<td>1.97</td>
<td><p>T</p>
<p>(TBD)</p></td>
<td>Manufacturers data - Marotta</td>
</tr>
<tr class="odd">
<td>Warm Helium Supply COPV</td>
<td><p>8.3</p>
<p>(506)</p></td>
<td><p>200</p>
<p>(2900)</p></td>
<td>Al 2219, Carbon Fibre</td>
<td>300</td>
<td>244(3538)</td>
<td>See Note 13</td>
<td>610(8845)</td>
<td><h1 id="section-24">2.5</h1></td>
<td>2.5</td>
<td><p>500</p>
<p>(7250)</p></td>
<td>2.05</td>
<td><p>T</p>
<p>(TBD)</p></td>
<td>Manufacturers drawing / data</td>
</tr>
<tr class="even">
<td>Cryogenic pilot valve tubing. See Note 11 for all fittings</td>
<td><p>&lt;10</p>
<p>(&lt;610)</p></td>
<td>6 (87)</td>
<td>316 SS Grade A</td>
<td><p>300</p>
<p>1.8</p></td>
<td><p>11 (159.5)</p>
<p>11 (159.5)</p></td>
<td>See Note 1</td>
<td><p>1485 (21532)</p>
<p>3714 (53853)</p></td>
<td><h1 id="section-25">4</h1></td>
<td><p>185</p>
<p>464</p></td>
<td>16.5 (239.3)</td>
<td>1.5</td>
<td>A</td>
<td>SCL – AMS-02 Pressure system parts.xls</td>
</tr>
<tr class="odd">
<td>Warm pilot valve tubing. See Note 11 for all fittings</td>
<td><p>&lt;10</p>
<p>(&lt;610)</p></td>
<td>6 (87)</td>
<td>316 SS Grade A</td>
<td>300</td>
<td>10 (145)</td>
<td>See Note 1</td>
<td>1485 (21532)</td>
<td><h1 id="section-26">4</h1></td>
<td>185</td>
<td>16.5 (239.3)</td>
<td>1.5</td>
<td>A</td>
<td>SCL – AMS-02 Pressure system parts.xls</td>
</tr>
<tr class="even">
<td>Tube from COPV to DV22, and MV42. See Note 11 for fittings</td>
<td><p>&lt;10</p>
<p>(&lt;610)</p></td>
<td>200 (2900)</td>
<td>AISI 316 L</td>
<td>300</td>
<td>244(3538)</td>
<td>See Note 13</td>
<td><p>1739</p>
<p>(25215)</p></td>
<td><h1 id="section-27">4</h1></td>
<td>7.13</td>
<td>480 (6960)</td>
<td>1.97</td>
<td>A</td>
<td>SCL – AMS-02 Pressure system parts.xls</td>
</tr>
<tr class="odd">
<td>Tube from DV22 to MV40 valves</td>
<td><p>&lt;10</p>
<p>(&lt;610)</p></td>
<td>200 (2900)</td>
<td>AISI 316 L</td>
<td>300</td>
<td>244(3538)</td>
<td>See Note 13</td>
<td><p>1739</p>
<p>(25215)</p></td>
<td><h1 id="section-28">4</h1></td>
<td>7.13</td>
<td>480 (6960)</td>
<td>1.97</td>
<td>A</td>
<td>SCL – AMS-02 Pressure system parts.xls</td>
</tr>
<tr class="even">
<td>Tube from MV40 to PS01 and PS02</td>
<td><p>&lt;10</p>
<p>(&lt;610)</p></td>
<td>6 (87)</td>
<td>AISI 316 L</td>
<td>300</td>
<td>8 (116)</td>
<td>See Note 1</td>
<td><p>1739</p>
<p>(25215)</p></td>
<td><h1 id="section-29">4</h1></td>
<td>217</td>
<td>12 (174)</td>
<td>1.5</td>
<td>A</td>
<td>SCL – AMS-02 Pressure system parts.xls</td>
</tr>
<tr class="odd">
<td>PS01 and PS02</td>
<td><p>&lt;10</p>
<p>(&lt;610)</p></td>
<td>6 (87)</td>
<td>AISI 316 L</td>
<td>300</td>
<td>8 (116)</td>
<td>See Note 1</td>
<td><p>&gt;20</p>
<p>(&gt;290)</p></td>
<td><h1 id="section-30">2.5</h1></td>
<td>&gt;2.5</td>
<td>20 (290)</td>
<td>2.5</td>
<td>T (TBD manufacturer)</td>
<td>United Electronic Controls Drawing E17W-H97</td>
</tr>
<tr class="even">
<td>Tube from PS01 and PS02 to warm pilot valves</td>
<td><p>&lt;10</p>
<p>(&lt;610)</p></td>
<td>6 (87)</td>
<td>AISI 316 L</td>
<td>300</td>
<td>8 (116)</td>
<td>See Note 1</td>
<td><p>693</p>
<p>(10048.5)</p></td>
<td><h1 id="section-31">2.5</h1></td>
<td>86</td>
<td>12 (174)</td>
<td>1.5</td>
<td>T (TBD)</td>
<td>SCL – AMS-02 Pressure system parts.xls</td>
</tr>
<tr class="odd">
<td>Tube from PS01 and PS02 to cold pilot valves</td>
<td><p>&lt;10</p>
<p>(&lt;610)</p></td>
<td>6 (87)</td>
<td>AISI 316 L</td>
<td>300</td>
<td>8 (116)</td>
<td>See Note 1</td>
<td><p>1485</p>
<p>(21532.5)</p></td>
<td><h1 id="section-32">2.5</h1></td>
<td>185</td>
<td>12 (174)</td>
<td>1.5</td>
<td>T (TBD)</td>
<td>SCL – AMS-02 Pressure system parts.xls</td>
</tr>
<tr class="even">
<td><p>Warm Weka valves actuation bellows for</p>
<p>DV09A – B</p>
<p>DV11A – B</p>
<p>DV15A – D</p>
<p>DV16A – B</p></td>
<td><p>&lt;10</p>
<p>(&lt;610)</p></td>
<td>6 (87)</td>
<td>St St 316Ti/ EN1.4571</td>
<td>300</td>
<td>8 (116)</td>
<td>See Note 1</td>
<td><p>&gt;20</p>
<p>(&gt;290)</p></td>
<td><h1 id="section-33">2.5</h1></td>
<td>&gt;2.5</td>
<td>8.8 (127.6)</td>
<td>1.1</td>
<td>T (Weka)</td>
<td>Weka qualification and acceptance tests of warm valves</td>
</tr>
<tr class="odd">
<td>Pilot valve vacuum vessel (PVVV)</td>
<td>4.0</td>
<td>-1 (-14.5)</td>
<td><p>Stainless Steel</p>
<p>304-S12</p></td>
<td>300</td>
<td>10 (145)</td>
<td>See Note 1</td>
<td>91.5 (1326.7)</td>
<td><h1 id="section-34">2.5</h1></td>
<td>9</td>
<td><p>15</p>
<p>(217.5)</p></td>
<td>1.5</td>
<td><p>A</p>
<p>See Note 9</p>
<p>T(TBD)</p></td>
<td>SCL – AMS-02 Pressure system parts.xls</td>
</tr>
<tr class="even">
<td>Tube from PVVV to DV20 Valves</td>
<td><p>&lt;10</p>
<p>(&lt;610)</p></td>
<td>-1 (-14.5)</td>
<td>AISI 316 L</td>
<td>300</td>
<td>10 (145)</td>
<td>See Note 1</td>
<td>1739 (25215)</td>
<td><h1 id="section-35">2.5</h1></td>
<td>174</td>
<td><p>15</p>
<p>(217.5)</p></td>
<td>1.5</td>
<td>T (TBD)</td>
<td></td>
</tr>
<tr class="odd">
<td>Tube from MV43 to PVVV</td>
<td><p>&lt;10</p>
<p>(&lt;610)</p></td>
<td>-1 (-14.5)</td>
<td>AISI 316 L</td>
<td>300</td>
<td>10 (145)</td>
<td>See Note 1</td>
<td>2080 (30160)</td>
<td><h1 id="section-36">2.5</h1></td>
<td>208</td>
<td><p>15</p>
<p>(217.5)</p></td>
<td>1.5</td>
<td>T (TBD)</td>
<td></td>
</tr>
<tr class="even">
<td>Tube from PVVV to MV44</td>
<td><p>&lt;10</p>
<p>(&lt;610)</p></td>
<td>-1 (-14.5)</td>
<td>AISI 316 L</td>
<td>300</td>
<td>10 (145)</td>
<td>See Note 1</td>
<td>2080 (30160)</td>
<td><h1 id="section-37">2.5</h1></td>
<td>208</td>
<td><p>15</p>
<p>(217.5)</p></td>
<td>1.5</td>
<td>T (TBD)</td>
<td></td>
</tr>
<tr class="odd">
<td><p>Warm valve pilot valves</p>
<p>DV61AS-BS</p>
<p>DV61AO-BO</p>
<p>DV66AS-BS</p>
<p>DV66AO-BO</p>
<p>DV59AS-BS</p>
<p>DV59AS-BO</p>
<p>DV65AS-DS</p>
<p>DV65AO-DO</p></td>
<td><p>&lt;10</p>
<p>(&lt;610)</p></td>
<td>6 (87)</td>
<td>PAA GF60, Brass, Spring Steel, Steel, Nitric Rubber, POM,
Aluminium</td>
<td>300</td>
<td>8 (116)</td>
<td>See Note 1</td>
<td><p>&gt;20</p>
<p>(&gt;290)</p></td>
<td><h1 id="section-38">2.5</h1></td>
<td>&gt;2.5</td>
<td>12 (174)</td>
<td>&gt;1.5</td>
<td><p>T</p>
<p>(TBD)</p></td>
<td></td>
</tr>
<tr class="even">
<td><p>Relief valve</p>
<p>RV03</p></td>
<td><p>&lt;10</p>
<p>(&lt;610)</p></td>
<td>6 (87)</td>
<td>6061 T6 Al. Aly., 316 SST, VESPEL SP1, 320 SST, TEFLON</td>
<td>300</td>
<td><p>Fault:</p>
<p>8 (116)</p></td>
<td>See Note 1</td>
<td>24.8 (365)</td>
<td><h1 id="section-39">2.5</h1></td>
<td>3.1</td>
<td>15 (217.5)</td>
<td>1.8</td>
<td>-</td>
<td>See Manufacturers Qualification Docs (TBD)</td>
</tr>
<tr class="odd">
<td><p>Relief valve</p>
<p>RV04</p></td>
<td><p>&lt;10</p>
<p>(&lt;610)</p></td>
<td>6 (87)</td>
<td>6061 T6 Al. Aly., 316 SST, VESPEL SP1, 320 SST, TEFLON</td>
<td>300</td>
<td><p>Fault:</p>
<p>8 (116)</p></td>
<td>See Note 1</td>
<td>24.8 (359.6)</td>
<td><h1 id="section-40">2.5</h1></td>
<td>3.1</td>
<td>15 (217.5)</td>
<td>1.8</td>
<td>-</td>
<td>See Manufacturers Qualification Docs (TBD)</td>
</tr>
<tr class="even">
<td>Vent Pump</td>
<td>TBD</td>
<td>-1 (-14.5)</td>
<td>TBD</td>
<td>300</td>
<td>10 145)</td>
<td>See Note 1</td>
<td>TBD</td>
<td><h1 id="section-41">2.5</h1></td>
<td>TBD</td>
<td>11 (159.5)</td>
<td>1.1</td>
<td>T</td>
<td>Manufacturer’s Qualification</td>
</tr>
<tr class="odd">
<td>Barometric Switch</td>
<td><p>&lt;&lt;10</p>
<p>(&lt;610)</p></td>
<td>0.02 (0.29)</td>
<td>2024 T4 Aluminium, Ni-SPAN-C Alloy</td>
<td>300</td>
<td>1 (14.5)</td>
<td>-</td>
<td>&gt;2.5 (&gt;36.25)</td>
<td><h1 id="section-42">2.5</h1></td>
<td>&gt;2.5</td>
<td>2.04 (29.6)</td>
<td>2.04</td>
<td>-</td>
<td>See Manufacturers Qualification Docs (TBD)</td>
</tr>
</tbody>
</table>

### Note 1: Derivation of MDP values per NSTS 1700.7B and ISS Addendum, section 208.4

The maximum design pressure (MDP) for all systems considered in this
report is set by the upper defined limit of the relevant pressure relief
device which is a space-qualified bursting disc or relief valve.

The bursting disc systems have been extensively assessed by LM/NASA and
SCL and accepted.

a.  3 bar Pressure Relief

b.  

The pressure is set by the upper limit on the differential pressure,
when cold, necessary to rupture bursting disc BD03, shown on SCL
Cryogenic System Schematic Drawing SCD 1000.

In service and in test, the downstream pressure on this disc is kept at
zero bar absolute.

> In the warm state, the bursting disc will rupture at less than 3 bar.

c.  20 bar Pressure Relief

d.  

The pressure is set by the upper limit on the differential pressure,
when cold, necessary to rupture bursting disc BD02, shown on SCL
Cryogenic System Schematic Drawing SCD 1000.

Although in service the downstream pressure is \~ 10 mbar (fill vacuum),
the design allows for the downstream pressure being 3 bar abs. The
superfluid cooling loop SCL is thus designed for 23 bar abs (and
differential), whereas the bursting disc BD02 is set for a maximum
differential of 20 bar, in the cold state.

In the warm state, the bursting disc BD02 will rupture at less than 22
bar differential.

e.  10 bar Pressure Relief

f.  

The pressure is set by the upper limit on the burst disc differential
pressure and vacuum case vacuum, when cold, necessary to rupture
bursting discs BD05A, BD05B, BD10A, BD11A,BD11B, BD12A, BD12B, BD13
shown on SCL Cryogenic System Schematic Drawing SCD 1000.

Although in service the pipework pressure is \< 1.0 bar, the design
allows for the trapped volume pressures being up to 11 bar abs. (10 bar
differential of the bursting disc failing to atmosphere + 1 bar vacuum
in the Vacuum Case) The general pipework is thus designed for 11 bar abs
(and differential), whereas the bursting discs listed are set for a
maximum differential of 10 bar.

g.  RV03 / RV04

h.  

RV03 and RV04 relief valves operate in parallel, nominal cracking
pressure is 7.5 bar and full flow occurs at 8 bar. MDP has been
established using the full flow value.

Note 2: Materials of pressure-containing part.

Note 3: Basis for verification of Burst Safety Factor.

Note 4: This is a vacuum vessel and the MDP only applies in the event of
contingency case.

Note 5: Ground Case - Worst case thermal pressure environment caused by
rupture of the Super Fluid He Tank into the Vacuum Case.

Note 6: Pressure on upstream side of disc, absolute.

Note 7: For all items in this table, the designed on-orbit life is: 3
years + 2 contingency years. Expected life is TBD as the AMS-02 does not
have an independent means of end of life disposal from the ISS.

Note 8: Proof pressure is based upon current specification for valve
fittings and will be updated when valves are ordered to meet
requirements of 1.5 times MDP.

Note 9: Current pilot valve vacuum vessel design based upon calculations
in BS 5500. Vessel will be proof tested to 16.5 bar once manufactured.

Note 10: Actuation, hence pressurisation can only occur when DV22A -- D
are open; therefore MDP determination set by RV04 due to two relief
valves being present in the system.

Note 11: Any fittings are designed to have a minimum wall thickness
equivalent to the pipework they are connecting.

Note 12: A proof pressure of 1.1 MDP is applicable to all bi-metallic
feedthroughs as they will be pressure tested with the helium vessel and
not prior to this. Analysis shows that factors of safety against burst
are tens of times greater than MDP therefore a 1.1 proof test is deemed
acceptable.

Note 13: MDP Determined by controlling the fill of warm helium gas as
per SCL memo 2906 Control of Warm Helium Gas System Fill_Rev04.pdf dated
4^th^ April 2007.

![](media/image2.jpeg){width="8.99236111111111in" height="5.275in"}

### Cryomagnet System

![](media/image3.jpeg){width="7.364583333333333in"
height="6.028472222222222in"}

### Warm Helium Supply and Pilot Valve Details Enlarged

  ----------------------------------------------------- ---------------------------------------------------- ----------------------------------------------------
  ![](media/image5.jpeg){width="4.591666666666667in"                                                         ![](media/image6.jpeg){width="3.272222222222222in"
  height="5.958333333333333in"}                                                                              height="5.833333333333333in"}

  **Weka Cryogenic Valve (Cold Valve)**                                                                      

  ![](media/image8.jpeg){width="3.8333333333333335in"   ![](media/image9.jpeg){width="5.583333333333333in"   
  height="5.519444444444445in"}                         height="3.401388888888889in"}                        

  **Weka Warm Valves (Addressed in AMS-02-F05)**                                                             
  ----------------------------------------------------- ---------------------------------------------------- ----------------------------------------------------

# Table 3: Cryosystem Burst Disks

+----------------+--------+------+---------+---------+---------------+
| Subsystem      | System | Nu   | Relief  | Relief  | "Vent To"     |
|                | ID     | mber | P       | P       | Location      |
|                |        | of   | ressure | ressure |               |
|                |        | D    |         |         |               |
|                |        | isks | (bar)   | (psi)   |               |
+----------------+--------+------+---------+---------+---------------+
| Main Helium    | BD03,  | 3 in | 3       | 43.5    | Out of AMS-02 |
| Tank           | BD06A, | se   |         |         |               |
|                | BD06B  | ries | (Outer  |         | Emergency     |
|                |        |      | BD set  |         | Helium Vent   |
|                |        |      | to 2    |         |               |
|                |        |      | bar to  |         |               |
|                |        |      | account |         |               |
|                |        |      | for     |         |               |
|                |        |      | atmo    |         |               |
|                |        |      | spheric |         |               |
|                |        |      | p       |         |               |
|                |        |      | ressure |         |               |
|                |        |      | and     |         |               |
|                |        |      | ev      |         |               |
|                |        |      | acuated |         |               |
|                |        |      | line)   |         |               |
+----------------+--------+------+---------+---------+---------------+
| Vacuum Vessel  | BD07A, | 3 in | 0.8     | 11.6    | Out of AMS-02 |
|                | BD07B, | se   |         |         |               |
|                | BD07C  | ries |         |         |               |
+----------------+--------+------+---------+---------+---------------+
| Main Helium    | BD05A, | 2 in | 10      | 145     | Out of AMS-02 |
| Tank --        | BD05B  | se   |         |         |               |
| Through        |        | ries |         |         |               |
| Pourous Plug   |        |      |         |         |               |
+----------------+--------+------+---------+---------+---------------+
| Liquid Helium  | BD13A, | 2 in | 10      | 145     | Out of AMS-02 |
| Fill Port      | BD13B  | se   |         |         |               |
|                |        | ries |         |         |               |
+----------------+--------+------+---------+---------+---------------+
| Vapor Cooled   | BD10A, | 2 in | 10      | 145     | Out of AMS-02 |
| Leads          | BD10B  | se   |         |         |               |
|                |        | ries |         |         |               |
+----------------+--------+------+---------+---------+---------------+
| Cold Buffer    | BD11A, | 2 in | 10      | 145     | Out of AMS-02 |
| Volume/        | BD11B  | se   |         |         |               |
| Superfluid     |        | ries |         |         |               |
| Cooling Loop   |        |      |         |         |               |
+----------------+--------+------+---------+---------+---------------+
| Cold Buffer    | BD02,  | 2    | 20      | 290     | Main Helium   |
| Volume/        |        |      |         |         | Tank,         |
| Superfluid     | BD18   |      |         |         |               |
| Cooling Loop   |        |      |         |         | Out of AMS-02 |
+----------------+--------+------+---------+---------+---------------+
| Cool Down      | BD12A, | 2 in | 10      | 145     | Out of AMS-02 |
| Circuit        | BD12B  | se   |         |         |               |
|                |        | ries |         |         |               |
+----------------+--------+------+---------+---------+---------------+

+----------------------------+-----------------------------------------+
| ![](media/image10.png){wi  | ![](media/im                            |
| dth="3.5284722222222222in" | age12.jpeg){width="5.190972222222222in" |
| hei                        | height="3.8930555555555557in"}          |
| ght="4.513888888888889in"} |                                         |
+----------------------------+-----------------------------------------+
|                            | The burst disk numbers are as follows:  |
|                            | SCL designation (BD..) followed by Fike |
|                            | disk number (SK\...).                   |
|                            |                                         |
|                            | BD02, BD18 - SK2456-2 Rev B             |
|                            |                                         |
|                            | BD03 - SK2456-6 Rev E                   |
|                            |                                         |
|                            | BD05, BD10, BD11, BD12, BD13, BD17 -    |
|                            | SK2456-4 Rev D                          |
|                            |                                         |
|                            | BD06 - SK2456-7 Rev D                   |
|                            |                                         |
|                            | BD07 - SK2456-5 Rev B                   |
+----------------------------+-----------------------------------------+
| **Cryogenic System Burst   |                                         |
| Disk**                     |                                         |
|                            |                                         |
| The burst disk             |                                         |
| manufacturer is **Fike**.  |                                         |
| (UK, 35 Earl Street,       |                                         |
| Maidstone, Kent, ME14 1PF, |                                         |
| Tel +44 (0) 1622 677081 \| |                                         |
| US, Tel +1 816 229 3405.)  |                                         |
+----------------------------+-----------------------------------------+
| **Tested Burst Disk**      | ![](media/im                            |
|                            | age13.jpeg){width="5.069444444444445in" |
|                            | height="4.940277777777778in"}           |
+----------------------------+-----------------------------------------+

  ---------------------------------------------------- -----------------------------------------------------
  ![](media/image14.png){width="4.627777777777778in"   ![](media/image15.png){width="4.4944444444444445in"
  height="5.941666666666666in"}                        height="5.897222222222222in"}

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

  ---------------------------------------------------- ----------------------------------------------------
  ![](media/image16.png){width="4.493055555555555in"   ![](media/image17.png){width="4.639583333333333in"
  height="6.50625in"}                                  height="6.472916666666666in"}

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

![](media/image18.png){width="5.642361111111111in"
height="6.495833333333334in"}

## Fracture Classification for AMS-02 Cryomagnet

  ---------------- ------------ ----------- ----------- --------- ----------- -------- ---------------- ----------- --------------
  Item             Drawing      Material    Material    Max.      Ratio of    Margin   Fracture         Rationale   Comments
                   Number       and temper  allowable   applied   applied     of       Classification               
                                            stress      tensile   limit       Safety                                
                                            (ksi)       stress    stress to   (ult) FS                              
                                                        (ksi)     allowable   =1.50                                 
                                                                  stress                                            

  Race track End   SCD0825      6061-T6 (10 53.7        29.4      0.55        0.22     Low risk         Note 2      Page 7,
  frame                         in)                                                                                 sect.1.1.1
                                                                                                                    Note 4

  Dipole Island    SCD0810      6061-T6 (10 53.7        29.0      0.54        0.23     Low risk         Note 2      Page
                                in)                                                                                 8,sect.1.1.2 c
                                                                                                                    Note 4

  Race track coils SCD0841      6061-T6 (10 53.7        19.6      0.37        0.83     Low risk         Note 2      Page
                                in)                                                                                 8,sect.1.1.2 b
                                                                                                                    Note 4

  Race track edge  SCD0851-4    2219-T851   60.9        27.6      0.45        0.47     Low risk         Note 2      Page 13,sect
  plate outer                                                                                                       1.1.5 a, max.
                                                                                                                    tens stress
                                                                                                                    preload warm,
                                                                                                                    Note 4

  Race track edge  SCD0851-3    6061-T6 (10 53.7        21.6      0.40        0.14     Low risk         Note 2      Page 13,sect
  plate curved                  in)                                                                                 1.1.5 b, max.
                                                                                                                    tens stress
                                                                                                                    preload warm,
                                                                                                                    Note 4

  Dipole edge      SCD0812-01   6061-T6 (10 53.7        22.5      0.42        0.10     Low risk         Note 2      Page 14,sect
  Plate                         in)                                                                                 1.1.5 c, max.
                                                                                                                    tens stress
                                                                                                                    preload warm,
                                                                                                                    Note 4

  Helium vessel Fx SCD0889-02   316 Hi      232.1       143.6     0.62        0.08     Low risk         Note 2      Page 47, sect
  support pin                   proof                                                                               4.1.d inertia
                                stainless                                                                           loads, Note 4
                                steel                                                                               

  Helium vessel Fy SCD0910-01   316 Hi      31.9        20.5      0.64        0.42     Low risk         Note 2      Page 49, sect
  support pin                   proof                                         yield                                 4.2.A inertia
                                stainless                                                                           loads, Note 4
                                steel                                                                               

  Helium vessel Fz SCD0898-01   316 Hi      232.1       130.7     0.56        0.18     Low risk         Note 2      Page 54, sect
  support pin                   proof                                                                               4.4.C inertia
                                stainless                                                                           loads, Note 4
                                steel                                                                               

  **Fasteners**                                                                                                     

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

  RT1 to RT3 bolts SCD0842-01   A4/70, M8   3702        2534      0.68        0.46     Fail-safe        Note 3      Page 2,
                                316                                           yield                                 Appendix 5
                                stainless                                                                           Note 4
                                steel                                                                               

  RT3 to RT5 bolts SCD0845-04   A4/70, M12  8527        5666      0.66        0.50     Fail-safe        Note 3      Page 2,
                                316                                           yield                                 Appendix 5
                                stainless                                                                           Note 4
                                steel                                                                               

  RTEF to RT5      SCDXXX       M8, 316 Hi  6129        2468      0.40        1.48     Fail-safe        Note 3      Page 2,
  bolts                         proof                                         yield                                 Appendix 5
                                stainless                                                                           Note 4
                                steel                                                                               

  Dipole crossbeam SCD0815      UNF 316 Hi  17417       3758      0.22        3.63     Fail-safe        Note 3      Page 2,
  to RTEF bolts                 proof                                         yield                                 Appendix 5
                                stainless                                                                           Note 4
                                steel                                                                               

  Dipole island to SCD0824      M5, 316 Hi  2378        1114      0.47        1.14     Fail- safe       Note 3      Page 2,
  RTEF bolts                    proof                                         yield                                 Appendix 5
                                stainless                                                                           Note 4
                                steel                                                                               

  Dipole edge      SCD0824      M5, 316 Hi  2378        1166      0.49        1.04     Fail- safe       Note 3      Page 2,
  plate to RTEF                 proof                                         yield                                 Appendix 5
  bolts                         stainless                                                                           Note 4
                                steel                                                                               

  Helium vessel Fz SCD0898      M8, 316 Hi  6129        3313      0.54        0.85     Fail- safe       Note 3      Page 2,
  support bolts                 proof                                         yield                                 Appendix 5
                                stainless                                                                           Note 4
                                steel                                                                               

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

## Fracture Classification of AMS-02 Helium Tank

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

  Central Ring     SCD 0905-01   5083-H111   32.6        28.2      0.86        0.05     Non Fracture     Note 2      Page 18
                                 forging                                                critical                     Note 3

  Thru tube weld   SCD 0903-02   5083-H111   25.89       23.4      0.90        0.01     Non Fracture     Note 2      Page 18
                                 forging                                                critical                     Note 3

  Outer ring       SCD           5083-H321   25.52       17.7      0.69        0.31     Non Fracture     Note 2      Page18
                   0905-02,-03                                                          critical                     Note 3

  Inner ring weld  SCD           5083-H321   25.52       20.3      0.79        0.14     Non Fracture     Note 2      Page 18
                   0905-04,-05                                                          critical                     Note 3

  Porous plug weld SCD 0905-22   5083-H321   25.89       20.7      0.80        0.13     Non Fracture     Note 2      Page18
                                                                                        critical                     Note 3

  End dish weld    SCD 0906      5083-H321   25.52       14.0      0.55        0.66     Non fracture     Note 2      Page 18
                                                                                        critical                     Note 3

  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                                                                                                      
  assessment, July                                                                                                   
  24, 2003                                                                                                           
  ---------------- ------------- ----------- ----------- --------- ----------- -------- ---------------- ----------- ----------

## Fracture Classification for AMS-02 Cryomagnet Suspension Straps

  ---------------- --------- ----------- ----------- --------- ----------- -------- ---------------- ----------- ------------------
  Item             Drawing   Material    Material    Max.      Ratio of    Margin   Fracture         Rationale   Comments
                   Number    and temper  allowable   applied   applied     of       Classification               
                                         stress      tensile   limit       Safety                                
                                         (ksi)       stress    stress to   (ult) FS                              
                                                     (ksi)     allowable   =1.40                                 
                                                               stress                                            

  Race track end   SCD0825   6061-T6 (10 13.69       4.43      0.32        0.11     Fracture         Note 2,3    Page 7, Note 5
  frame clevis               in)                                                    critical                     RTEF_C1W1_clevis

  Race track end   SCD       316L        127.64      85.77     0.67        0.06     Fracture         Note 2,3    Page 13, Note 5
  frame clevis pin 0678-02   Hi-Proof                                               critical                     RTEF_C1W1_clevis
                             stainless                                                                           
                             steel                                                                               

  Carbon Band      SCD       Carbon      275.65      117.7     0.43        0.67     Fracture         Note 2,3    Note 4
                   0678-03   Fiber epoxy                                            critical                     

  FGR Band         SCD       FGR3 epoxy  261.07      59.3      0.22        2.14     Fracture         Note 2,3    Note 4
                   0678-12                                                          critical                     

  Glass Band       SCD       S2 glass    217.56      61.2      0.28        1.53     Fracture         Note 2,3    Note 4
                   0678-11   epoxy                                                  critical                     

  Glass Bod        SCD       S2 glass    217.56      98.3      0.45        0.58     Fracture         Note 2,3    Note 4
                   0678-18   epoxy                                                  critical                     

  Notes:                                                                                                         

  1\) The                                                                                                        
  components will                                                                                                
  be calassified                                                                                                 
  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, 6                                                                                                    
  February 2002                                                                                                  

  5\) Ref.                                                                                                       
  Cryomagnet                                                                                                     
  Suspension Strap                                                                                               
  Analysis                                                                                                       
  ---------------- --------- ----------- ----------- --------- ----------- -------- ---------------- ----------- ------------------

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