SATPC0037414 Tab 04 4 SOW_Redacted.pdf
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- This is for a procurement for 10 CC Closed Bombs Federal contract opportunity
- Solicitation number
- 80NSSC25893469Q
About this file
This Statement of Work (SOW) outlines requirements for manufacturing the Fixture, 10 CC bomb assembly (SEB26100021-205) for NASA Johnson Space Center (JSC), which is used in qualification testing of the NASA Standard Initiator to measure pressure versus time curves.
The contractor must manufacture 35 units of SEB26100021-007 and 30 units of SEB26100021-008, with delivery required within 12 weeks after receipt of order. Key requirements include: contractor-supplied raw materials from a single heat lot with single heat treatment, maintaining traceability throughout manufacturing, compliance with NASA drawing SEB26100021 Rev H specifications, and meeting SKH26152127 Rev D supplier requirements. NASA-JSC will provide thread gages and perform certain tasks including impression stamping and volumetric checks. The contractor must individually package all hardware to prevent damage during shipping, provide all relevant documentation and certifications, and deliver to NASA JSC in Houston, TX. No first article units are required.
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Other files for this federal contract opportunity
| File | Type | Posted |
|---|---|---|
| SATPC0037414 Tab 04 Drawings.pdf | ||
| SATPC0037414 Tab 10 RFQ Open Market.pdf |
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Text version
STATEMENT OF WORK 09/17/24
FOR THE MANUFACTURE OF THE
FIXTURE, 10 CC BOMB
1.0 SCOPE
1.1 Fabrication requirements.
The Contractor shall manufacture the Fixture, 10 CC bomb in accordance with the requirements of this statement of work (SOW) and NASA-JSC drawing SEB26100021 Rev H.
NASA-JSC will perform impression stamping of parts, flag notes 2 and 12.
NASA-JSC will perform volumetric checks of assemblies flag note 7.
1.2 Hardware Description.
Fixture, 10 CC bomb assembly SEB26100021-205 is used in qualification testing of the NASA Standard Initiator (NSI) where pressure verses time curves are measured to verify proper function.
2.0 TECHNICAL REQUIREMENTS
2.1 Prospective Suppliers.
Suppliers bidding for this contract must meet the requirements of drawing SKH26152127 Rev D.
2.2 Design Requirements.
All design requirements are listed on NASA-JSC drawing SEB26100021 Rev H.
2.3 Quantity and Delivery Schedule.
ITEM QUANTITY UNIT DELIVERY SCHEDULE
SEB26100021-007 35 EA 12 WEEKS ARO
SEB26100021-008 30 EA 12 WEEKS ARO
3.0 PROGRAM MANAGEMENT REQUIREMENTS
3.1 Raw material requirements.
Raw material for this production run shall be supplied by the contractor.
3.2 Production / Traceability requirements.
The Contractor shall maintain traceability of each production part to the original heat lot number from which it was machined throughout the manufacturing process.
All parts listed on this SOW shall be from a single heat lot of material and single heat treat.
3.3 Thread Gages.
Go / No-go thread gages for this production run will be supplied by NASA-JSC
3.4 First Article Requirements.
No first article units are required by NASA-JSC.
3.5 Production Acceptance Requirements
All production articles shall be inspected and verified to comply with NASA drawing SEB26100021 Rev H and the workmanship standards specified. Inspection shall take place at both the Contractor facility and NASA-JSC for final acceptance.
3.6 Documentation Requirements
The Contractor shall furnish documentation indicating compliance with all required drawing specifications. Work performed by sub-contractors i.e. heat treating shall be documented by subcontractor certifications and test reports as applicable and copies provided to NASA-JSC with the deliverables.
4.0 SAFETY REQUIREMENTS
The Contractor shall comply with all Federal, State and Local codes and standards applicable to work performed on this contract.
5.0 APPLICABLE DOCUMENTS
DOCUMENT NUMBER REV DOCUMENT TITLE
SEB26100021 H Fixture, 10 CC bomb
SAE-AMS-5643 Latest Rev Steel, Corrosion-Resistant, Bars, Wire, Forgings, Tubing, and Rings 16Cr - 4.0Ni - 0.30Cb (Nb) - 4.0Cu Solution Heat Treated, Precipitation Hardenable
SAE-AS5202 Latest Rev Port or fitting end, internal Straight thread Design standard.
ASTM E18 Latest Rev Standard Test Methods for Rockwell Hardness of Metallic Materials
SKH26152127 D Approved Supplier List for Aerospace Material Machined Parts.
6.0 SHIPPING, PRESERVATION AND PACKAGING REQUIREMENTS
The Contractor shall individually package all deliverable pieces of hardware such that during transportation the hardware cannot get damaged if subjected to above average road vibrations or rough handling.
The Contractor shall supply NASA-JSC copies of all applicable paperwork associated with this production run.
The Contractor shall ship all deliverable pieces of hardware to:
NASA/Lyndon B. Johnson Space Center Transportation Officer, Bldg 421
2101 NASA Parkway Houston, TX. 77058
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