**[PROPOSAL INSTRUCTIONS]{.underline}: \_X\_ DRAFT \-- COMMENTS DUE BY:
11/29/06 COB**

> **[\_­\_]{.underline} FINAL \-- PROPOSAL DUE BY: 12/15/06 COB**

**[DO TITLE]{.underline}: EVA Enhanced Right Angle Drive**

**DO Type: [\_ X\_]{.underline} CPFF [\_\_\_]{.underline} FFP**

**[DO Contact Information in Addition to the CRAVE Contract Specialist
or CO]{.underline}:**

**TMR: [Joe Gensler]{.underline} Phone: [(281) 483-0025]{.underline}**

**DO Manager: [David Glebe]{.underline} Phone: [(281)
483-9216]{.underline}**

**DO Mgr. Alternate: Phone: [\_\_\_\_\_\_\_\_\_\_\_\_\_]{.underline}**

**[Concurrences]{.underline}:**

**[\_\_\_\_]{.underline} [\_\_\_\_]{.underline} [\_\_\_\_]{.underline}**

**David Glebe Harold Reimers Joe Gensler**

**DO Manager DO Mgr. Management COTR**

**[\_\_\_\_]{.underline} [\_\_\_\_]{.underline} [\_\_\_\_]{.underline}**

**Joe Gensler Steve Miller Mary F. Thomas**

**Division TMR S & MA Contract Specialist**

**Task Contains Flight Hardware, Flight Software or GSE? [\_
X\_]{.underline} Yes [\_\_\_]{.underline}No**

**Program Supported: [\_X\_]{.underline}Shuttle [\_X]{.underline} ISS
[\_X\_]{.underline}EVA [\_ \_]{.underline}Advanced**

**\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\--**

**WBS: [\_X\_]{.underline} 1.0 EVA [\_\_]{.underline} 2.0 FCE
[\_\_]{.underline} 3.0 EVR [\_\_]{.underline} ECLSS [\_\_]{.underline}
5.0 ATCS [\_\_]{.underline} 6.0 CHeCS**

# 

*For purposes of complying with FAR 52.232-22, Limitation of Funds, the
total amount allotted by the Government to contract is specified in
clause B.6, Contract Funding. The funding listed in B.6 is the amount
allotted for **all** Delivery Orders on the contract combined.*

*All terms and conditions of the contract apply to this Delivery Order.
In the event of a conflict between the contract and this Delivery Order,
the contract shall prevail.*

*WBS reporting shall be done in accordance with applicable WBS reporting
categories, as shown above and in the contract within Section C, Table
1.*

# **[Narrative Task Description]{.underline}**

## [Background / Problem Description]{.underline}:

## 

1.  [Objective]{.underline}

The existing bilateral tool Right Angle Drive (P/N SEG33106925-305) has
revealed early cycle life issues that restrict the useful life and
impact overall confidence in the output torque values. Design, develop,
certify, manufacture, and deliver an Enhanced Right Angle Drive (ERAD)
that is suitable for breaking and applying static torques and to use as
a continuous torque transmission device.

2.  [Need for an Enhanced Right Angle Drive]{.underline}

The Right Angle Drive (P/N: SEG33106925-305) that is currently being
used in International Space Station (ISS) assembly tasks was only
designed to remove ninety-six (96) bolts that would require no more than
five (5) turns each. Since the RADs initial certification, ISS assembly
teams have determined that the RAD needs to be used in other assembly
tasks that include driving bolts in excess of five (5) turns as well as
performing final bolt torques. Thus, a new "enhanced" right angle drive
is required to complete ISS assembly tasks.

3.  [Prior Work]{.underline}

NASA currently uses a Right Angle Drive (P/N: SEG33106925-301/-303/-305)
that was not designed to be used as a transmission to continuously drive
bolts more than five (5) turns. The current design was extensively fit
checked to worksites (at the vendor facilities) throughout the
development of ISS. The existing RAD dimensions are believed to be
acceptable for the RAD to be used in all assembly tasks which require
the use of the RAD.

## [Task Description]{.underline}: 

The contractor is to perform the necessary analysis and design of the
ERAD to meet the performance requirements as listed below. The
contractor shall present a design concept to NASA prior to being awarded
the contract to design, fabricate, and certify the ERAD. Upon approval
of the design by NASA, the contractor shall complete the design,
fabrication, testing, and certification of the ERAD. The design shall
comply with applicable EVA GDRD requirements. The contractor shall, upon
successful completion of testing, manufacture, and certification,
deliver one (1) qualification, five (5) flight, no (0) Neutral Buoyancy
Laboratory (NBL) compatible ERADs and provide sustaining engineering as
required for the hardware for a period of no less than two (2) years. No
part of the design will be proprietary and NASA will have full access
and ownership of all engineering drawings, CAD models, procedures, and
related documentation. The drawings will be released in the Electronic
Drawing Control Center. All drawings will use JSC standard processing
(i.e., PRC) callouts. All documentation (requirements documents,
assembly procedures, etc) will be released through the JSC document
system.

1.  **[Requirements]{.underline}**

The ERAD shall meet, at minimum, the requirements that are listed in
JSC-33601, Revision J for the Right Angle Drive (P/N: SEG33106925-305)
with the following exceptions:

*[Weight]{.underline}*

-   The weight of the ERAD shall not exceed 2.8 pounds.

*[Dimensions]{.underline}*

-   The ERAD shall not exceed the following envelope dimensions:

    -   Stowed (handle closed): 10.83 in. x 2.5 in. x 3.10 in.

    -   Deployed (handle extended): 10.83 in. x 2.5 in. x 7.25 in.

-   Additional envelope dimension constraints:

    -   The output housing of the ERAD should not exceed 1.5 inches in
        diameter

*[Interfaces]{.underline}*

The enhanced right angle drive (ERAD) shall interface with the
following: EVA standard 3/8" male drives and EVA standard female drop
proof tethers (DPTs). These interfaces shall function with a maximum
100^ο^F differential over the operational temperature range.

-   Extravehicular Activity Standard 3/8" Male Drive Interface

    -   Orientation

        -   Interface of the ERAD EVA standard 3/8" male drive to the
            DPT shall be independent of orientation.

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    -   Interface Definition

        -   Interface to the ERAD EVA standard 3/8" male drive shall be
            in accordance with ICD JSC-33546 (CTSD-SS-1035).

    -   3/8" Drive Gage

        -   The ERAD output drive shall interface with the 3/8" male
            drive go and no-go gage (SDG38114280-001).

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-   Drop Proof Tether (DPT) Interface

    -   Orientation

        -   Interface of the ERAD DPT to the EVA standard 3/8" male
            drive shall be independent of orientation.

    -   Interface Definition

        -   Interface of the ERAD DPT shall be in accordance with ICD
            JSC-33546 (CTSD-SS-1035).

    -   Drop Proof Tether Gage

        -   The ERAD DPT shall interface with the DPT go and no-go gage
            (SDG38114281-001) and the McTether load fixture (gage)
            (SDG38114296-001).

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-   Push-In-Place (PIP) Pin Interface

    -   Interface Definition

        -   Interface to the standard 3/16" PIP pin shall be in
            accordance with ICD JSC-33546 (CTSD-SS-1035).

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    ```
    -   Push-In-Place (PIP) Pin Gage

        -   The ERAD DPT shall interface with the DPT PIP pin gage
            (SDG38114295-001).

*[Life Cycling of ERAD Mechanism]{.underline}*

-   Drive Mechanism Cycling

    -   The total number of output cycles are derived as follows :

        -   2 drive tasks/EVA x 10 cycles/drive task x 31 EVAs/year x 15
            years x F.S. \[where F.S. = 2.0\] = 18,600 cycles

    -   The 3/8" male drive shall be capable of withstanding (at
        minimum) 18,600 cycles to verify life expectancy. A cycle is
        defined as one clockwise (CW) turn followed by one
        counterclockwise (CCW) turn. (NOTE: it is acceptable to perform
        (for acceptance/qualification testing) large number of cycles as
        follows: 100 CW cycles followed by 100 CCW cycles.)

        -   CCW: Break bolt torque with a 28.1 ft-lbs (25.5 ft-lbs x
            1.10) ERAD input load

        -   CCW: Drive bolt 100 turns with a bolt running torque (ERAD
            output load) of 2.0 ft-lbs.

        -   CW: Drive bolt 100 turns with an bolt running torque (ERAD
            output load) of 2.0 ft-lbs.

        -   CW: Final bolt torque with a 28.1 ft-lbs (25.5 ft-lbs x
            1.10) ERAD input load.

    -   The above cycle profile (100 cycles) shall be repeated until the
        required number of cycles are achieved.

    -   Life cycle testing may be interrupted to allow the ERAD to cool

-   Male Drive Cycling

    -   The ERAD male drive shall be capable of withstanding 1860 cycles
        to verify life expectancy (1 tool change out/task x 2 tasks/EVA
        x 31 EVAs/year x 15 years x F.S. \[where F.S. = 2.0\].

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```
-   Drop Proof Tether (DPT) Mechanism

    -   The DPT drive shall be capable of withstanding 5580 cycles to
        verify life expectancy (3 DPT change outs/task x 2 tasks/EVA x
        31 EVAs/year x 15 years x F.S. \[where F.S. = 2.0\].

-   Handle Deployment Cycling

    -   The handle shall be capable of withstanding 1860 cycles to
        verify life expectancy (1 handle deployment/task x 2 tasks/EVA x
        31 EVAs/year x 15 years x F.S. \[where F.S. = 2.0\]).

*[Loads]{.underline}*

-   The ERAD shall be able to meet all of the load and cycle
    requirements over the full operational temperature range of it\'s
    certification.

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-   The design/analysis/testing of the ERAD shall include thermal
    degradation factors based on the predicted temperature range of the
    ERAD.

-   At the end of the useful life of useful life of the ERAD, the torque
    transmission efficiency shall not be less than 1.5:1 (output: input)
    for both static and dynamic load conditions.

-   Torque multiplication factor cannot change by more than 0.4 over the
    life of the tool. This may be described by the equation (*beginning
    of life - end of life* [\<]{.underline} .4).

-   The rotational input speed (at no-load conditions) shall not exceed
    sixty (60) revolutions per minute (RPM).

-   The rotational input speed shall not exceed sixty (60) RPM when the
    output torque is driving a bolt with a two (2.0) foot-pound (ft-lb)
    running torque.

-   The maximum input static load shall not exceed 36.6 ft-lbs (30.5
    ft-lbs x 1.20).

-   The maximum dynamic input load shall not exceed 28.1 ft-lbs (25.5
    ft-lbs x 1.10).

    -   The cooling time shall be determined through thermal analysis
        and/or testing but shall not exceed five (5) minutes based on
        EVA environments extremes

-   The ERAD shall be designed such that no debris (i.e., Foreign Object
    Debris \[FOD\]) will be generated during the life of the tool

*[Operational Forces]{.underline}*

-   The retention force of the DPT locked on an EVA standard 3/8" male
    drive shall be 18.0 pounds (limit) without functional degradation of
    the system components. The DPT shall retain an EVA standard 3/8"
    male drive for a minimum of 60.0 pounds (ultimate).

-   3/8" Male Drive Soft Docking Force

    -   The force required to soft dock into a DPT shall measure between
        0.5 and 2.5 pounds.

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-   Handle Actuation Force

    -   The force required to open/close the ERAD handle shall measure
        between 1.0 and 6.0 pounds (measured at the center of the
        handle).

-   PIP Pin Actuation Force

    -   The force required to insert or remove the PIP pin into or out
        of the ERAD DPT shall measure between 0.25 and 3.5 pounds.

*[Functional Requirements]{.underline}*

-   Fastener Installation and Removal

    -   ERAD shall be capable of performing breaking torque on
        fasteners, driving the fastener (during installation or
        removal), and performing final fastener torque.

-   Drive Mechanism Capability

    -   The ERAD shall allow a continuous rotation in the clockwise and
        counterclockwise directions. The mechanism shall operate freely.

-   Torque Output Angle

    -   The ERAD output drive axis shall be perpendicular to the input
        drive axis.

-   Output-to-Input Rotation

    -   The ERAD shall have an output drive rotational direction that is
        the same as the input drive rotational direction.

-   Handle Lock

    -   The ERAD handle shall be capable of being deployed and locked in
        eight (8) positions (in 45 degree increments) around the ERAD
        drive train.

-   Handle Position

    -   The ERAD handle shall be stowable, and shall have at minimum at
        least two (2) detent positions (0 degrees \[fully stowed\] and
        90 degrees \[fully deployed\]).

2.  **[Reporting]{.underline}**

The contractor shall provide weekly technical status, a bi-monthly
schedule review, and monthly financial management reports as directed in
the data requirements table.

3.  **[Earned Value]{.underline}**

The contractor shall provide data pertaining to earned value reporting
for the milestones identified in the "Interim Milestones" Table.

4.  **[Government Provided Equipment]{.underline}**

See Government Furnished Property section.

5.  **[Project Management Plan]{.underline}**

The contractor is not required to generate a Project Management Plan
(PMP).

**[Deliverables/Products]{.underline}:**

+---------------+---------------------------+-------+-------+----------+
| #             | ###### Description        | ##### | ##### | ####     |
| ##### Product |                           | # Qty | # Due | ## Class |
+---------------+---------------------------+-------+-------+----------+
| **Hardware**  |                           |       |       |          |
+---------------+---------------------------+-------+-------+----------+
| Mock Up       |                           |       |       |          |
+---------------+---------------------------+-------+-------+----------+
| Prototype     | Functional Prototype for  | 1     | 5     | III      |
|               | engineering testing       |       | /1/07 |          |
+---------------+---------------------------+-------+-------+----------+
| Certification | Full Class I Flight       |       |       |          |
|               | certification including   |       |       |          |
|               | thermal, load and         |       |       |          |
|               | vibration                 |       |       |          |
+---------------+---------------------------+-------+-------+----------+
| Flight        | Full acceptance testing   | 5     |       | I        |
+---------------+---------------------------+-------+-------+----------+
| Training      | N/A                       |       |       |          |
+---------------+---------------------------+-------+-------+----------+
| Other         | Qualification Unit        | 1     |       | I/II     |
+---------------+---------------------------+-------+-------+----------+
| #####         |                           |       |       |          |
+---------------+---------------------------+-------+-------+----------+
| ##### Test    | Functional testing        | N/A   |       | I / qual |
|               | (acceptance and           |       |       |          |
|               | qualification)            |       |       |          |
+---------------+---------------------------+-------+-------+----------+
| #####         |                           |       |       |          |
+---------------+---------------------------+-------+-------+----------+
| **Software**  | N/A                       | N/A   | N/A   | N/A      |
+---------------+---------------------------+-------+-------+----------+
|               |                           |       |       |          |
+---------------+---------------------------+-------+-------+----------+
| **Other       | Acceptance Data Package   | 1 per |       | I / II   |
| Products**    | (ADP) for each flight and | each  |       |          |
|               | qualification units       | f     |       |          |
|               |                           | light |       |          |
|               |                           | /     |       |          |
|               |                           | qual  |       |          |
|               |                           | unit  |       |          |
+---------------+---------------------------+-------+-------+----------+
| **Other       | GCAR                      | 1     | 8/    | N/A      |
| Products**    |                           |       | 28/08 |          |
+---------------+---------------------------+-------+-------+----------+
|               |                           |       |       |          |
+---------------+---------------------------+-------+-------+----------+

########  

######## SCHEDULE

######## 

######## Start Date: February 5, 2007 Finish Date: July 25, 2008

########  

  ----------------------------------- -----------------------------------
  **ITERIM MILESTONES**               **DUE DATES**

  **System Requirements Review        **Suggested date 3/1/07**
  (SRR)**                             

  **Prototype Fabricated**            **Suggested date 5/1/07**

  **Prototype Testing Completed**     **Suggested date 6/1/07**

  **Preliminary Design Review (PDR)** **Suggested date 6/15/07**

  **Critical Design Review (CDR)**    **Suggested date 10/16/07**

  **Hardware Fabrication Complete**   **Suggested date 2/15/08**

  **Hardware Qual / Acceptance        **Suggested date 5/16/08**
  Testing Complete**                  

  **Certification Complete**          **Suggested date 6/17/08**

  **SAR**                             **Suggested date 7/1/08**

  **Hardware Delivery**               **7/25/08**

  **Milestones, along with subjective 
  measurements, are to be used for    
  measuring performance. For schedule 
  detail see Microsoft Project file   
  located on the CRAVE web site for   
  this DO listed under the Government 
  Cost Estimate below.**              
  ----------------------------------- -----------------------------------

**[Government Estimate Located in RFQ File in Microsoft Project File On
CRAVE Web Site]{.underline}**

**[The file is titled]{.underline}: EVA Electric CIPA gun.mpp**

**Total Government Estimate for this DO:**
[[\$1200K]{.underline}]{.mark}

**Option 1:** [\$\_\_\_]{.underline} **(See Attachment 1)**

**Option 2: [\$]{.underline} (See Attachment 2)**

**TOTAL COST ESTIMATE FOR THIS DO: [[\$(Contractor Complete)
]{.underline}]{.mark}**

**FEE: [[\$]{.underline}]{.mark} (If Applicable)**

**OPTION 1: [[\$ N/A]{.underline}]{.mark} (See Attachment 1)**

**OPTION 2: [[\$ N/A]{.underline}]{.mark} (See Attachment 2)**

**[DATA REQUIREMENTS]{.underline}**

> **Notes: 1. Grey Scaled Rows Need No Additional/Required Fill-ins.**
>
> **2. On all other rows, If Necessary, Fill in Additional**
>
> Rqmts/Deliveries in last Column.

+---+-----+------------------+---------+----------+-------+----------+
| * | **D | **DRD TITLE**    | **DUE** | **FRE    | **    | **CO     |
| * | ATA |                  |         | QUENCY** | REQUI | MMENTS** |
| D | TYP |                  |         |          | RED** |          |
| R | E** |                  |         |          |       |          |
| D |     |                  |         |          | **FOR |          |
| \ |     |                  |         |          | DO?** |          |
| # |     |                  |         |          |       |          |
| * |     |                  |         |          | **    |          |
| * |     |                  |         |          | Y/N** |          |
+===+=====+==================+=========+==========+=======+==========+
| 1 | W   | Flight GFE       | With    | Once     | **    |          |
|   | rit | Configuration    | P       |          | Attac |          |
|   | ten | Management Plan  | roposal |          | hment |          |
|   | Ap  |                  |         |          | J-8** |          |
|   | pro |                  |         |          |       |          |
|   | val |                  |         |          |       |          |
+---+-----+------------------+---------+----------+-------+----------+
| 2 | Man | Regular Status   | Thirty  | Monthly  | **Y** | Weekly   |
|   | dat | Report/ Summary  | (30)    |          |       | Tech     |
|   | ory | Review           | days    |          |       | status   |
|   | Sub |                  | fo      |          |       |          |
|   | mit |                  | llowing |          |       |          |
|   | tal |                  | c       |          |       |          |
|   |     |                  | ontract |          |       |          |
|   |     |                  | start   |          |       |          |
+---+-----+------------------+---------+----------+-------+----------+
| 3 | W   | Project          | If      | Once     | **N** |          |
|   | rit | Technical        | R       | with     |       |          |
|   | ten | Requirements     | equired | R        |       |          |
|   | Ap  | Specification    | for DO  | evisions |       |          |
|   | pro |                  | See     |          |       |          |
|   | val |                  | C       |          |       |          |
|   |     |                  | omments |          |       |          |
+---+-----+------------------+---------+----------+-------+----------+
| 4 | Man | GFE Systems      | If      | Once     | **N** |          |
|   | dat | Requirements     | R       | with     |       |          |
|   | ory | Data Package     | equired | R        |       |          |
|   | Sub |                  | for DO  | evisions |       |          |
|   | mit |                  | See     |          |       |          |
|   | tal |                  | C       |          |       |          |
|   | if  |                  | omments |          |       |          |
|   | Flt |                  |         |          |       |          |
|   | H/W |                  |         |          |       |          |
+---+-----+------------------+---------+----------+-------+----------+
| 5 | W   | Flight GFE       | If      | Once     | **N** |          |
|   | rit | Projects         | R       | with     |       |          |
|   | ten | Requirements &   | equired | R        |       |          |
|   | Ap  | Verification     | for DO  | evisions |       |          |
|   | pro | Document         | See     |          |       |          |
|   | val |                  | C       |          |       |          |
|   |     |                  | omments |          |       |          |
+---+-----+------------------+---------+----------+-------+----------+
| 6 | Man | Preliminary      | If      | Once     | **Y** |          |
|   | dat | Design Review    | R       | with     |       |          |
|   | ory | Data Package     | equired | R        |       |          |
|   | Sub |                  | for DO  | evisions |       |          |
|   | mit |                  | See     |          |       |          |
|   | tal |                  | C       |          |       |          |
|   | if  |                  | omments |          |       |          |
|   | Flt |                  |         |          |       |          |
|   | H/W |                  |         |          |       |          |
+---+-----+------------------+---------+----------+-------+----------+
| 7 | W   | Flight GFE       | If      | Once     | **Y** |          |
|   | rit | Workmanship      | R       | with     |       |          |
|   | ten | Specifications   | equired | R        |       |          |
|   | Ap  | List             | for DO  | evisions |       |          |
|   | pro |                  | See     |          |       |          |
|   | val |                  | C       |          |       |          |
|   |     |                  | omments |          |       |          |
+---+-----+------------------+---------+----------+-------+----------+
| 8 | W   | Project Schedule | PDR or  | Once     | **Y** |          |
|   | rit |                  | 10%     | w/R      |       |          |
|   | ten |                  | effort  | evisions |       |          |
|   | Ap  |                  | c       | (due     |       |          |
|   | pro |                  | omplete | w/DO     |       |          |
|   | val |                  | Mi      | p        |       |          |
|   |     |                  | lestone | roposal, |       |          |
|   |     |                  |         | updates  |       |          |
|   |     |                  |         | &        |       |          |
|   |     |                  |         | details  |       |          |
|   |     |                  |         | provided |       |          |
|   |     |                  |         | as DO    |       |          |
|   |     |                  |         | pro      |       |          |
|   |     |                  |         | gresses) |       |          |
+---+-----+------------------+---------+----------+-------+----------+
| 9 | W   | Flight GFE       | If      | Once     | **Y** |          |
|   | rit | Interface        | R       | with     |       |          |
|   | ten | Control Document | equired | R        |       |          |
|   | Ap  |                  | for DO  | evisions |       |          |
|   | pro |                  | See     |          |       |          |
|   | val |                  | C       |          |       |          |
|   |     |                  | omments |          |       |          |
+---+-----+------------------+---------+----------+-------+----------+
| 1 | W   | GFE End Item     | If      | Once     | **N** |          |
| 0 | rit | Specification    | R       | with     |       |          |
|   | ten |                  | equired | R        |       |          |
|   | Ap  |                  | for DO  | evisions |       |          |
|   | pro |                  | See     |          |       |          |
|   | val |                  | C       |          |       |          |
|   |     |                  | omments |          |       |          |
+---+-----+------------------+---------+----------+-------+----------+
| 1 | Man | Flight GFE       | If      | As       | **Y** |          |
| 1 | dat | Failure Analysis | R       | Required |       |          |
|   | ory | Report           | equired |          |       |          |
|   | Sub |                  | for DO  |          |       |          |
|   | mit |                  | See     |          |       |          |
|   | tal |                  | C       |          |       |          |
|   | if  |                  | omments |          |       |          |
|   | Flt |                  |         |          |       |          |
|   | H/W |                  |         |          |       |          |
+---+-----+------------------+---------+----------+-------+----------+
| 1 | W   | Flight GFE       | As      | Once     | **Y** |          |
| 2 | rit | Verification and | Sp      | with     |       |          |
|   | ten | Validation Plan  | ecified | R        |       |          |
|   | Ap  |                  | in      | evisions |       |          |
|   | pro |                  | WI      |          |       |          |
|   | val |                  | -EA-023 |          |       |          |
+---+-----+------------------+---------+----------+-------+----------+
| 1 | W   | GFE Software     | If      | Once     | **N** |          |
| 3 | rit | Requirements     | R       | with     |       |          |
|   | ten | Specification    | equired | R        |       |          |
|   | Ap  |                  | for DO  | evisions |       |          |
|   | pro |                  | See     |          |       |          |
|   | val |                  | C       |          |       |          |
|   |     |                  | omments |          |       |          |
+---+-----+------------------+---------+----------+-------+----------+
| 1 | W   | GFE Software     | If      | Once     | **N** |          |
| 4 | rit | Development Plan | R       | with     |       |          |
|   | ten |                  | equired | R        |       |          |
|   | Ap  |                  | for DO  | evisions |       |          |
|   | pro |                  | See     |          |       |          |
|   | val |                  | C       |          |       |          |
|   |     |                  | omments |          |       |          |
+---+-----+------------------+---------+----------+-------+----------+
| 1 | W   | GFE Software     | If      | As       | **N** |          |
| 5 | rit | Design Document  | R       | Required |       |          |
|   | ten |                  | equired |          |       |          |
|   | Ap  |                  | for DO  |          |       |          |
|   | pro |                  | See     |          |       |          |
|   | val |                  | C       |          |       |          |
|   |     |                  | omments |          |       |          |
+---+-----+------------------+---------+----------+-------+----------+
| 1 | W   | Engineering      | If      | Once     | **Y** | Pro-E    |
| 6 | rit | Drawings         | R       | with     |       | format   |
|   | ten |                  | equired | R        |       | CAD      |
|   | Ap  |                  | for DO  | evisions |       | Models   |
|   | pro |                  | See     |          |       | and      |
|   | val |                  | C       |          |       | Drawing  |
|   |     |                  | omments |          |       | files    |
+---+-----+------------------+---------+----------+-------+----------+
| 1 | W   | EEE Parts Lists  | If      | As       | **N** | No EEE   |
| 7 | rit | and Analysis     | R       | Required |       | parts    |
|   | ten | Report           | equired |          |       |          |
|   | Ap  |                  | for DO  |          |       |          |
|   | pro |                  | See     |          |       |          |
|   | val |                  | C       |          |       |          |
|   |     |                  | omments |          |       |          |
+---+-----+------------------+---------+----------+-------+----------+
| 1 | Man | Critical Design  | If      | Once     | **Y** |          |
| 8 | dat | Review Data      | R       | with     |       |          |
|   | ory | Package          | equired | R        |       |          |
|   | Sub |                  | for DO  | evisions |       |          |
|   | mit |                  | See     |          |       |          |
|   | tal |                  | C       |          |       |          |
|   | if  |                  | omments |          |       |          |
|   | Flt |                  |         |          |       |          |
|   | H/W |                  |         |          |       |          |
+---+-----+------------------+---------+----------+-------+----------+
| 1 | Man | Engineering      | If      | As       | **Y** |          |
| 9 | dat | Drawing Change   | R       | Required |       |          |
|   | ory | Proposal         | equired |          |       |          |
|   | Sub |                  | for DO  |          |       |          |
|   | mit |                  | See     |          |       |          |
|   | tal |                  | C       |          |       |          |
|   | if  |                  | omments |          |       |          |
|   | Flt |                  |         |          |       |          |
|   | H/W |                  |         |          |       |          |
+---+-----+------------------+---------+----------+-------+----------+
| 2 | W   | GFE              | If      | Once     | **Y** |          |
| 0 | rit | Qualification    | R       | with     |       |          |
|   | ten | Test Procedure   | equired | R        |       |          |
|   | Ap  |                  | for DO  | evisions |       |          |
|   | pro |                  | See     |          |       |          |
|   | val |                  | C       |          |       |          |
|   |     |                  | omments |          |       |          |
+---+-----+------------------+---------+----------+-------+----------+
| 2 | W   | Flight Product   | If      | Once     | **N** |          |
| 1 | rit | User's Guide     | R       | with     |       |          |
|   | ten |                  | equired | R        |       |          |
|   | Ap  |                  | for DO  | evisions |       |          |
|   | pro |                  | See     |          |       |          |
|   | val |                  | C       |          |       |          |
|   |     |                  | omments |          |       |          |
+---+-----+------------------+---------+----------+-------+----------+
| 2 | Man | Software Code    | If      | As       | **N** |          |
| 2 | dat |                  | R       | Required |       |          |
|   | ory |                  | equired |          |       |          |
|   | Sub |                  | for DO  |          |       |          |
|   | mit |                  | See     |          |       |          |
|   | tal |                  | C       |          |       |          |
|   | if  |                  | omments |          |       |          |
|   | Flt |                  |         |          |       |          |
|   | H/W |                  |         |          |       |          |
+---+-----+------------------+---------+----------+-------+----------+
| 2 | W   | Information      | \(30\)  | JPG      | **    |          |
| 3 | rit | Technology (IT)  | days    | 2810.1   | Attac |          |
|   | ten | Security Program | after   |          | hment |          |
|   | Ap  | Plan and Reports | DO      |          | J-4** |          |
|   | pro |                  | award,  |          |       |          |
|   | val |                  | and as  |          | **Due |          |
|   |     |                  | sp      |          | 30    |          |
|   |     |                  | ecified |          | days  |          |
|   |     |                  | in JPG  |          | after |          |
|   |     |                  | 2810.1  |          | DO    |          |
|   |     |                  |         |          | aw    |          |
|   |     |                  |         |          | ard** |          |
+---+-----+------------------+---------+----------+-------+----------+
| 2 | W   | Certification    | If      | Once     | **Y** |          |
| 4 | rit | Plan             | R       | with     |       |          |
|   | ten |                  | equired | R        |       |          |
|   | Ap  |                  | for DO  | evisions |       |          |
|   | pro |                  | See     |          |       |          |
|   | val |                  | C       |          |       |          |
|   |     |                  | omments |          |       |          |
+---+-----+------------------+---------+----------+-------+----------+
| 2 | Man | Certification    | If      | Once     | **Y** |          |
| 5 | dat | Report           | R       | with     |       |          |
|   | ory |                  | equired | R        |       |          |
|   | Sub |                  | for DO  | evisions |       |          |
|   | mit |                  | See     |          |       |          |
|   | tal |                  | C       |          |       |          |
|   | if  |                  | omments |          |       |          |
|   | Flt |                  |         |          |       |          |
|   | H/W |                  |         |          |       |          |
+---+-----+------------------+---------+----------+-------+----------+
| 2 | Man | Engineering      | If      | As       | **Y** | [        |
| 6 | dat | Analysis         | R       | Required |       | ]{.mark} |
|   | ory |                  | equired |          |       |          |
|   | Sub |                  | for DO  |          |       |          |
|   | mit |                  | See     |          |       |          |
|   | tal |                  | C       |          |       |          |
|   | if  |                  | omments |          |       |          |
|   | Flt |                  |         |          |       |          |
|   | H/W |                  |         |          |       |          |
+---+-----+------------------+---------+----------+-------+----------+
| 2 | Man | Acceptance Data  | If      | One Time | **Y** | Supplied |
| 7 | dat | Package          | R       |          |       | for qual |
|   | ory |                  | equired |          |       | and      |
|   | Sub |                  | for DO  |          |       | Flight   |
|   | mit |                  | See     |          |       | Units    |
|   | tal |                  | C       |          |       |          |
|   | if  |                  | omments |          |       |          |
|   | Flt |                  |         |          |       |          |
|   | H/W |                  |         |          |       |          |
+---+-----+------------------+---------+----------+-------+----------+
| 2 | Man | Export Control   | After   | Yearly   | **Y** |          |
| 8 | dat | Audit Results    | award   |          |       |          |
|   | ory |                  | of 1st  |          |       |          |
|   | Sub |                  | DO,     |          |       |          |
|   | mit |                  | yearly  |          |       |          |
|   | tal |                  | on      |          |       |          |
|   |     |                  | Sept.   |          |       |          |
|   |     |                  | 30      |          |       |          |
|   |     |                  | the     |          |       |          |
|   |     |                  | reafter |          |       |          |
+---+-----+------------------+---------+----------+-------+----------+
| 2 | W   | Quality Plan     | With    | Once     | **    | Only if  |
| 9 | rit |                  | P       | with     | Attac | co       |
|   | ten |                  | roposal | R        | hment | ntractor |
|   | Ap  |                  |         | evisions | J     | is using |
|   | pro |                  |         |          | -11** | the      |
|   | val |                  |         |          |       | R        |
|   |     |                  |         |          |       | -quality |
|   |     |                  |         |          |       | plan     |
|   |     |                  |         |          |       | template |
|   |     |                  |         |          |       | instead  |
|   |     |                  |         |          |       | of ISO,  |
|   |     |                  |         |          |       | and only |
|   |     |                  |         |          |       | if they  |
|   |     |                  |         |          |       | need to  |
|   |     |                  |         |          |       | make     |
|   |     |                  |         |          |       | changes  |
|   |     |                  |         |          |       | to it.   |
+---+-----+------------------+---------+----------+-------+----------+
| 3 | W   | Patent           | As      | As       | **Y** |          |
| 0 | rit | Rights-Retention | R       | Required |       |          |
|   | ten |                  | equired |          | **(If |          |
|   | Ap  |                  |         |          | App   |          |
|   | pro |                  |         |          | licab |          |
|   | val |                  |         |          | le)** |          |
+---+-----+------------------+---------+----------+-------+----------+
| 3 | W   | Shuttle/Station  | If      | As       | **N** |          |
| 1 | rit | Payload Safety   | R       | Required |       |          |
|   | ten | Data Package     | equired |          |       |          |
|   | Ap  |                  | for DO  |          |       |          |
|   | pro |                  | See     |          |       |          |
|   | val |                  | C       |          |       |          |
|   |     |                  | omments |          |       |          |
+---+-----+------------------+---------+----------+-------+----------+
| 3 | Man | Limited Life     | If      | As       | **Y** |          |
| 2 | dat | Systems List     | R       | Required |       |          |
|   | ory |                  | equired |          |       |          |
|   | Sub |                  | for DO  |          |       |          |
|   | mit |                  | See     |          |       |          |
|   | tal |                  | C       |          |       |          |
|   | if  |                  | omments |          |       |          |
|   | Flt |                  |         |          |       |          |
|   | H/W |                  |         |          |       |          |
+---+-----+------------------+---------+----------+-------+----------+
| 3 | W   | Space Station    | If      | As       | **Y** | **If     |
| 3 | rit | GFE Failure      | R       | Required |       | appl     |
|   | ten | Modes and        | equired |          |       | icable** |
|   | Ap  | Effects Analysis | for DO  |          |       |          |
|   | pro | and Critical     | See     |          |       |          |
|   | val | Items List       | C       |          |       |          |
|   |     |                  | omments |          |       |          |
+---+-----+------------------+---------+----------+-------+----------+
| 3 | W   | Space Shuttle    | If      | As       | **N** | **If     |
| 4 | rit | GFE Safety and   | R       | Required |       | appl     |
|   | ten | Analysis Report  | equired |          |       | icable** |
|   | Ap  | &Hazard Report   | for DO  |          |       |          |
|   | pro |                  | See     |          |       |          |
|   | val |                  | C       |          |       |          |
|   |     |                  | omments |          |       |          |
+---+-----+------------------+---------+----------+-------+----------+
| 3 | W   | Software Quality | 90 Days | Once     | **N** |          |
| 5 | rit | Assurance Plan   | Prior   | with     |       |          |
|   | ten | Report           | to      | R        |       |          |
|   | Ap  |                  | S       | evisions |       |          |
|   | pro |                  | oftware |          |       |          |
|   | val |                  | Deve    |          |       |          |
|   |     |                  | lopment |          |       |          |
+---+-----+------------------+---------+----------+-------+----------+
| 3 | W   | ISS Hazard       | If      | As       | **Y** | **If     |
| 6 | rit | Report           | R       | Required |       | appl     |
|   | ten |                  | equired |          |       | icable** |
|   | Ap  |                  | for DO  |          |       |          |
|   | pro |                  | See     |          |       |          |
|   | val |                  | C       |          |       |          |
|   |     |                  | omments |          |       |          |
+---+-----+------------------+---------+----------+-------+----------+
| 3 | U   | Reliability and  | With    | One Time | **Y** |          |
| 7 | pon | Maintainability  | P       |          |       |          |
|   | R   | Plan             | roposal |          |       |          |
|   | equ |                  |         |          |       |          |
|   | est |                  |         |          |       |          |
+---+-----+------------------+---------+----------+-------+----------+
| 3 | W   | Government       | If      | As       | **Y** |          |
| 8 | rit | Certification    | R       | Required |       |          |
|   | ten | Approval Request | equired |          |       |          |
|   | Ap  | (GCAR)           | for DO  |          |       |          |
|   | pro |                  | See     |          |       |          |
|   | val |                  | C       |          |       |          |
|   |     |                  | omments |          |       |          |
+---+-----+------------------+---------+----------+-------+----------+
| 3 | W   | Risk Assessment  | If      | As       | **Y** |          |
| 9 | rit | Executive        | R       | Required |       |          |
|   | ten | Summary Report   | equired |          |       |          |
|   | Ap  | (RAESR)          | for DO  |          |       |          |
|   | pro |                  | See     |          |       |          |
|   | val |                  | C       |          |       |          |
|   |     |                  | omments |          |       |          |
+---+-----+------------------+---------+----------+-------+----------+
| 4 | W   | Problem          | 2       | As       | **Y** |          |
| 0 | rit | Reporting and    | b       | Required |       |          |
|   | ten | Corrective       | usiness |          |       |          |
|   | Ap  | Action (PRACA)   | days of |          |       |          |
|   | pro |                  | problem |          |       |          |
|   | val |                  | is      |          |       |          |
|   |     |                  | olation |          |       |          |
|   |     |                  | but no  |          |       |          |
|   |     |                  | later   |          |       |          |
|   |     |                  | than 10 |          |       |          |
|   |     |                  | days    |          |       |          |
|   |     |                  | after   |          |       |          |
|   |     |                  | de      |          |       |          |
|   |     |                  | tection |          |       |          |
+---+-----+------------------+---------+----------+-------+----------+
| 4 | U   | Nonconformance   | If      | As       | **Y** |          |
| 1 | pon | Record           | R       | Required |       |          |
|   | R   |                  | equired |          |       |          |
|   | equ |                  | for DO  |          |       |          |
|   | est |                  | See     |          |       |          |
|   |     |                  | C       |          |       |          |
|   |     |                  | omments |          |       |          |
+---+-----+------------------+---------+----------+-------+----------+
| 4 | Man | Government       | R       | Once     | **Y** |          |
| 2 | dat | Industry Data    | eported | with     |       |          |
|   | ory | Exchange Program | one     | R        |       |          |
|   | Sub | and NASA         | time    | evisions |       |          |
|   | mit | Advisory Problem | when    |          |       |          |
|   | tal | Data             | disc    |          |       |          |
|   |     |                  | repancy |          |       |          |
|   |     |                  | occurs  |          |       |          |
+---+-----+------------------+---------+----------+-------+----------+
| 4 | W   | Electrical,      | If      | Once     | **N** |          |
| 3 | rit | Electronic, and  | R       | with     |       |          |
|   | ten | Electromechnical | equired | R        |       |          |
|   | Ap  | (EEE) Parts      | for DO  | evisions |       |          |
|   | pro | Control Plan     | See     |          |       |          |
|   | val |                  | C       |          |       |          |
|   |     |                  | omments |          |       |          |
+---+-----+------------------+---------+----------+-------+----------+
| 4 | Man | Certification    | If      | Once     | **Y** |          |
| 4 | dat | Data Package     | R       | with     |       |          |
|   | ory |                  | equired | R        |       |          |
|   | Sub |                  | for DO  | evisions |       |          |
|   | mit |                  | See     |          |       |          |
|   | tal |                  | C       |          |       |          |
|   | if  |                  | omments |          |       |          |
|   | Flt |                  |         |          |       |          |
|   | H/W |                  |         |          |       |          |
+---+-----+------------------+---------+----------+-------+----------+
| 4 | W   | Certification    | At CDR  | Once     | **Y** |          |
| 5 | rit | and Acceptance   |         | with     |       |          |
|   | ten | Requirements     |         | R        |       |          |
|   | Ap  | Document         |         | evisions |       |          |
|   | pro |                  |         |          |       |          |
|   | val |                  |         |          |       |          |
+---+-----+------------------+---------+----------+-------+----------+
| 4 | U   | Wage/Salary and  | Thirty  | Once     | **N** |          |
| 6 | pon | Fringe Benefit   | (30)    |          |       |          |
|   | R   | Data             | days    |          |       |          |
|   | equ |                  | after   |          |       |          |
|   | est |                  | i       |          |       |          |
|   |     |                  | ssuance |          |       |          |
|   |     |                  | of each |          |       |          |
|   |     |                  | DO      |          |       |          |
+---+-----+------------------+---------+----------+-------+----------+
| 4 | W   | GFE Acceptance   | If      | One Time | **Y** |          |
| 7 | rit | Test Procedure   | R       |          |       |          |
|   | ten |                  | equired |          |       |          |
|   | Ap  |                  | for DO  |          |       |          |
|   | pro |                  | See     |          |       |          |
|   | val |                  | C       |          |       |          |
|   |     |                  | omments |          |       |          |
+---+-----+------------------+---------+----------+-------+----------+
| 4 | Man | Flight GFE       | If      | Once     | **Y** |          |
| 8 | dat | Verification &   | R       | with     |       |          |
|   | ory | Validation       | equired | R        |       |          |
|   | Sub | Report           | for DO  | evisions |       |          |
|   | mit |                  | See     |          |       |          |
|   | tal |                  | C       |          |       |          |
|   | if  |                  | omments |          |       |          |
|   | Flt |                  |         |          |       |          |
|   | H/W |                  |         |          |       |          |
+---+-----+------------------+---------+----------+-------+----------+
| 4 | Man | Space Shuttle    | If      | As       | **Y** | **If     |
| 9 | dat | GFE Failure      | R       | Required |       | appl     |
|   | ory | Modes and        | equired |          |       | icable** |
|   | Sub | Effects Analysis | for DO  |          |       |          |
|   | mit | (FMEA) and       | See     |          |       |          |
|   | tal | Critical Items   | C       |          |       |          |
|   | if  | List             | omments |          |       |          |
|   | Flt |                  |         |          |       |          |
|   | H/W |                  |         |          |       |          |
+---+-----+------------------+---------+----------+-------+----------+
| 5 |     | **Reserved**     | **      | *        | **\-  | *        |
| 0 |     |                  | \-\--** | *\-\--** | \--** | *\-\--** |
+---+-----+------------------+---------+----------+-------+----------+
| 5 | Man | NASA Contractor  | After   | Monthly  | **Y** |          |
| 1 | dat | Financial        | I       |          |       |          |
|   | ory | Management       | ssuance |          |       |          |
|   | Sub | Reporting        | of 1st  |          |       |          |
|   | mit |                  | DO      |          |       |          |
|   | tal |                  |         |          |       |          |
+---+-----+------------------+---------+----------+-------+----------+
| 5 | W   | Government       | With    | Once     | **    |          |
| 2 | rit | Property         | P       | with     | Attac |          |
|   | ten | Management Plan  | roposal | R        | hment |          |
|   | Ap  |                  |         | evisions | J-7** |          |
|   | pro |                  |         |          |       |          |
|   | val |                  |         |          |       |          |
+---+-----+------------------+---------+----------+-------+----------+
| 5 | Man | System Safety    | With    | One Time | **    |          |
| 3 | dat | Plan             | P       |          | Attac |          |
|   | ory |                  | roposal |          | hment |          |
|   | Sub |                  |         |          | J     |          |
|   | mit |                  |         |          | -10** |          |
|   | tal |                  |         |          |       |          |
+---+-----+------------------+---------+----------+-------+----------+
| 5 | W   | R-Quality Plan   | With    | Only     | **N** |          |
| 4 | rit | Template         | Pr      | ap       |       |          |
|   | ten |                  | oposal/ | plicable |       |          |
|   | Ap  |                  | Re      | to       |       |          |
|   | pro |                  | visions | B-CRAVE  |       |          |
|   | val |                  | as      | c        |       |          |
|   |     |                  | R       | ontracts |       |          |
|   |     |                  | equired | in       |       |          |
|   |     |                  |         | ac       |       |          |
|   |     |                  |         | cordance |       |          |
|   |     |                  |         | with the |       |          |
|   |     |                  |         | SOW and  |       |          |
|   |     |                  |         | the DRD  |       |          |
+---+-----+------------------+---------+----------+-------+----------+

Type 1 = Written Approval Type 2 = Mandatory Submittal Type 3 =
Submittal Upon Request

**[GOVERNMENT FURNISHED PROPERTY]{.underline}** - The list of items
below will be provided as Government Furnished Property.

  ---------------------------- ------------------------ -------------- -----------
  **Item**                     **Part Number**          **Quantity**   **Value**

  3/8" Male Drive Go/No-Go     SDG38114280-001          1              \$ 2000
  Gage                                                                 each

  DPT Go/No-Go Gage            SDG38114281-001          1              \$ 2000
                                                                       each

  McTether Load Fixture (Gage) SDG38114296-001          1              \$ 3000
                                                                       each

  DPT PIP Pin Gage             SDG38114295-001          1              \$ 2000
                                                                       each

                               **(available by October                 
                               15, 2007)**                             
  ---------------------------- ------------------------ -------------- -----------