SATPC0037886 Tab 04 4 SOW.pdf
PDF 113 KB Posted
- Attached to
- Standard off the shelf connectors, to support build up efforts for Orion Main Engine (OME)
- Solicitation number
- 80NSSC25898553Q
About this file
This Statement of Work (SOW) details NASA's requirement for electrical feedthrough interface connectors to support Orion Main Engine (OME) testing at NASA's White Sands Test Facility (WSTF) Propulsion Test Office. The project involves upgrading Test Stand 403 with specific connector types to enable engine level development, qualification, and acceptance testing for Artemis VI through IX vehicles.
The SOW specifies precise quantities and part numbers for seven different connector types, including instrumentation, controls, power, and NDAS mating connectors. Vendors must provide exactly matching parts, with any deviations requiring technical authority approval. The performance period is from March 1, 2025, through December 1, 2025, with work to be conducted at NASA JSC/WSTF Propulsion Test Office. The solicitation number is 80NSSC25898553Q and is issued by the National Aeronautics and Space Administration Shared Services Center.
View the file
Other files
| File | Type | Posted |
|---|---|---|
| SATPC0037886 Tab 10 Open Market RFQ.pdf |
On GovTribe
Work with this file
- Download the original file
- Contacts named in this file
- Similar government files
- Ask GovTribe AI about this file
Text version
STATEMENT OF WORK (Sample)
1. Objective/Requirements The scope of work is to provide the systems necessary hardware to perform engine level development, qualification and acceptance testing of the new Orion Main Engine (OME). The OME will be part of Orion Service Module and will be used on NASA’s Artemis VI through IX vehicles.
As part of this effort the obsolete electrical feedthroughs at NASA WSTF Propulsion test offices Test Stand 403 must be upgraded to meet the OME qualification and acceptance testing requirements.
2. Characteristics, Scope, and Specs Vender shall provide the electrical feedthrough interface connectors, listed in Table 1 to complete the updates to Test Stand 403. To meet propellant compatibility, flight hardware interface, and vacuum requirements the exact parts listed below must be provided. Any deviation must be approved by a technical authority at NASA WSTF Propulsion test office.
Table 1 Part# Description QT
D38999/26FE35SN Side A Instrumentation Feedthrough Mate 90 D38999/26FE35PN Side B Instrumentation Feedthrough Mate 90 D38999/26FE26SN Side A Controls Feedthrough Mate 90 D38999/26FE26PN Side B Controls Feedthrough Mate 90 D38999/26FE6SN Side A Power Feedthrough Mate 30 D38999/26FE6PN Side B Power Feedthrough Mate 30
D38999/26FC98PN NDAS Mating Connector 320
3. Place of Performance NASA JSC/WSTF Propulsion Test Office
4. Period of Performance Testing shall be performed March 1, 2025 through December 1, 2025.
File details come from the government source that posted it. Updated .