Advanced Cooling Techniques for Hydrocarbon Liquid Rocket Engine Components
Award amount
$749,998Program and phase
SBIR · Phase IIAward year
2004Award details
- Awarding agency
- Department of Defense
- Branch
- Air Force
- Recipient company
- METACOMP TECHNOLOGIES INC
- Proposal award date
- 2004-07-28
- Contract end date
- 2006-07-28
- UEI
- P1YHAJUA2G43
- Solicitation number
- 2003.2
- Topic code
- OSD03-009
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.
- Missile Plume Analysis & Modeling for Generation of Missile Profiles Used in Missile Warning
- Missile Plume Analysis and Modeling for Generation of Missile Profiles Used in Missile Warning
- Reliable Aerothermodynamic Predictions for Hypersonic Flight for High Speed ISR
- Multi-Phase Flame Propagation Modeling for Present and Future Combustors and Augmentors
- Modeling and Simulation of Lean Blowout in High-Pressure Swirl-Stabilized Combustors
Awards with the same topic code
Verified by an exact topic code match. This is not a text-similarity match.
- Advanced Cooling Techniques for Hydrocarbon Liquid Rocket Engine Components
- Oxygen Cooling of High Pressure Hydrocarbon Rocket Engines
- Full Scale Oxygen Rich Combustion Thrust Cell for Ejector Ramjets
Research funding history
40 SBIR/STTR records share this UEI (1995–2020). Reported award amounts total $13,861,836. Reported amounts are not federal obligations.
Phases: Phase I, Phase II
Agencies: Department of Defense