Enterprise High Speed Systems Test Technology (HSST)
Closed Pre-Solicitation Posted
- Solicitation number
- FA910125RHSST
- Agency
-
Air Force Test Center
Air Force Materiel Command, Department of Defense
- Responses due
- Set-aside
- No set-aside
Opportunity facts
- NAICS code
- 541715 Research and Development in the Physical, Engineering, and Life Sciences (except Nanotechnology and Biotechnology)
- PSC
- AC14 National Defense R&D Services; Department Of Defense - Military; R&D Administrative Expenses
- Place of performance
- Arnold AFB, Tennessee 37389, United States
Notice details come from SAM.gov. Updated .
About this opportunity
The Department of the Air Force Materiel Command Test Center (Air Force Test Center) is seeking research, testing, and evaluation of high-speed and hypersonic vehicle concepts, as well as analysis of supersonic and hypersonic vehicles and their components at true design conditions. This includes the evaluation of aerodynamic, aerothermal, aero-optics, aero-propulsion, jet interaction, and complex separation effects under relevant loads and at relevant scales. Vendors must perform a NIST SP 800-171 self-assessment and upload their score to the Supplier Performance Risk System (SPRS) in order to handle Controlled Unclassified Information (CUI) on their information systems. The draft Statement of Objectives is available to vendors who have completed the SPRS requirement.
This is a pre-solicitation notice, with no set-aside designations provided. The NAICS code is 541715 - Research and Development in the Physical, Engineering, and Life Sciences (except Nanotechnology and Biotechnology), and the PSC code is AC14-P - National Defense R&D Services; Department Of Defense - Military; R&D Administrative Expenses. The solicitation number is FA910125RHSST, and the deadline for questions and comments is August 23, 2024, though no award or proposal due dates are specified.
Notice text
Research, testing, and evaluation of high-speed and hypersonic vehicle concepts, and analysis of supersonic and hypersonic vehicles and their components at true design conditions. This includes the evaluation of aerodynamic, aerothermal, aero-optics, aero-propulsion, jet interaction, and complex separation effects under relevant loads and at relevant scales.
Files
| File | Type | Posted |
|---|---|---|
| 03 Attachment 2 Stakeholder Questions and Comments.xlsx | XLSX spreadsheet | |
| 03 Attachment 3 SPRS Requirements.docx | DOCX document |
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