SBIR/STTR Research Award
Rapid Design, Analysis, and Test of Hypersonic Propulsion Integrated Configurations
Award amount
$99,456Program and phase
SBIR · Phase IAward year
2008Award details
- Awarding agency
- Department of Defense
- Branch
- Air Force
- Recipient company
- ASTROX CORP
- Proposal award date
- 2007-12-28
- Contract end date
- 2008-10-29
- UEI
- G7DBH38ZAEQ8
- Solicitation number
- 2007.3
- Topic code
- AF073-091
Research abstract
The Air Force Research Laboratory Air Vehicles Directorate needs to be able to rapidly develop hypersonic vehicle concepts and to do so with as little risk as possible. A new technology called Rapid Prototyping will assist the Air Force in reducing risk in choosing the best path for fielding hypersonic vehicle systems. This technology will allow the rapid testing of many concepts, thus adding concrete knowledge to the design space and promoting good choices during early design stages.
Technology keywords
Not reported
Other awards by this recipient
Verified by the same UEI. These are other public SBIR/STTR award pages, not a merged company record.
- Micro Scale Testing of High Speed Aircraft
- Rapid Design, Analysis, and Test of Hypersonic Propulsion Integrated Configurations
- Flow Analysis Software Tool - SuperSIDE
- Combined-Cycle Engine Flow Path Analysis & Design Software Tool
- Analysis of Off-Design Considerations for Innovative Single-Stage-to-Orbit Configurations
Awards with the same topic code
Verified by an exact topic code match. This is not a text-similarity match.
- Combined Cycle Propulsion Integration
- Combined Cycle Propulsion Integration
- High-Speed Airbreathing Propulsion Integration
Research funding history
10 SBIR/STTR records share this UEI (1986–2012). Reported award amounts total $2,997,429. Reported amounts are not federal obligations.
Phases: Phase I, Phase II
Agencies: Department of Defense