Thermal Protection System (TPS) for Aggressive Reentry Trajectories of Space Vehicles
Award amount
$749,456Program and phase
SBIR · Phase IIAward year
2005Award details
- Awarding agency
- Department of Defense
- Branch
- Air Force
- Recipient company
- POWDERMET INC
- Proposal award date
- 2005-04-29
- Contract end date
- 2007-07-29
- UEI
- TK9JT3DMDW14
- Solicitation number
- 2004.1
- Topic code
- AF04-031
Research abstract
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.
- Development of Anisotropic Sintered NdFeB Magnet Consolidation Capacity
- Rapid Net Shape Fabrication of Complex Shapes
- Rare Earth Free Motor Designs with MnBi
- Rapid Manufacturing of Sintered NdFeB Permanent Magnets
- Thermally Engineered Gradient Refractory Metal Matrix Hot-Structures for Hypersonics
Awards with the same topic code
Verified by an exact topic code match. This is not a text-similarity match.
- Refractory Matrix Composites for CAV TPS
- Si-N-B-C Aerogels for Thermal Protection System of Reentry Vehicles
- Chemical Vapor Composite Materials for Thermal Protection Systems in Aggressive Reentry Space Vehicles
- Thermal Protection System (TPS) for Agressive Reentry Trajectories of Space Vehicles
- Refractory Matrix Composites for CAV TPS
Research funding history
123 SBIR/STTR records share this UEI (1998–2024). Reported award amounts total $29,889,391. Reported amounts are not federal obligations.
Phases: Phase I, Phase II, Phase II – Direct to Phase II
Agencies: Department of Defense, National Aeronautics and Space Administration, Department of Energy, National Science Foundation, Environmental Protection Agency, Department of Transportation