SATPC0033414 Tab 04 4 SOW.pdf
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- Attached to
- Hold-down and release mechanisms (HDRMs), part no. 061-005, quantity: 4 Federal contract opportunity
- Solicitation number
- 80NSSC24851177Q
About this file
This statement of work outlines requirements for electromechanically redundant hold-down release mechanisms for a lunar payload project. NASA Ames Research Center requires four medium duty HDRMs from Glenair, Inc. with part number 061-005 and a release preload of 2500lb. The devices will be used for deploying satellites and payloads in space, utilizing electrical current to break a fuse wire and release a pre-loaded bolt. The supplier must be ISO9001 compliant and provide certificates of conformance and traceability documentation. The hardware will support a Commercial Lunar Payload Services contract and be integrated at NASA Ames. The lead time is four weeks and products should ship to NASA Ames. Points of contact are provided for resource and program management. The related federal contract opportunity from the National Aeronautics and Space Administration Shared Services Center seeks these HDRMs with the same part number and quantity.
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Text version
Medium Duty HDRM Statement of Work
1. Suggested Supplier: Glenair, Inc.
2. Part Number: 061-005
3. Purchase Quantity: 4
4. Part Name: Electrically redundance Hold-Down Release Mechanism, Medium Duty.
2500lb release preload.
5. Part Description: Hold-Down and Release
Mechanisms are electromechanical devices used in the deployment of satellites and other payloads in space. Supplied in various formats and measured-release preloads, the devices are optimized for foolproof release-reliability with built-in mechanical and electrical redundancy. In non-pyrotechnic HDRMs, the planned release of the deployable satellite/payload is activated by a pre-determined value of electrical current to a fuse-wire system which causes the wire to break under tension and allows a pre-loaded mechanical bolt to actuate.
6. Purchase Notes
• Reference Glenair Quote #: RAH-23193549
• Supplier shall be in compliance with ISO9001
• Supplier shall provide Certificate of Conformance (CofC)
• Supplier shall provide lot/batch number, or other form of traceability
7. Planned Usage: Flight hardware for a lunar payload managed under the Commercial Lunar Payload Services (CLIPs) contract. Management, design, testing, and integration of the hardware will be done at NASA Ames Research Center.
8. Lead Time: 4wks ARO
9. Ship To:
NASA Ames Research Center Bldg. N213, Room 138 Moffett Field, CA 94035 ATT: Torin Bowman
(650) 450-3693
10. Points of Contact Resource Analyst:
Daniel Heacock, daniel.a.heacock@nasa.gov Program Manager:
Torin Bowman, torin.l.bowman@nasa.gov
Hold-Down Release Mechanism mailto:daniel.a.heacock@nasa.gov mailto:torin.l.bowman@nasa.gov
File details come from the government source that posted it. Updated .