Shock-Tube-Validated, Versatile Kinetic Mechanism Reduction Framework for Mixed Hydrocarbon-Based Rocket Fuels
Award amount
$749,984Program and phase
SBIR · Phase IIAward year
2022Award details
- Awarding agency
- Department of Defense
- Branch
- Air Force
- Recipient company
- ATA ENGINEERING, INC.
- Proposal award date
- 2022-09-19
- Contract end date
- 2024-12-20
- UEI
- PNZEUK9JC187
- Solicitation number
- 19.1
- Topic code
- AF191-068
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.
- Digital Engineering-Supported Characterization and Evaluation of Modern RF Aperture Materials
- A Machine Learning-Accelerated Framework for Lethality Assessment of Directed Energy Engagements of Hypersonic Threats
- Multiphysics Optimization of Mechanical Metamaterial Architectures
- Rapid AI-Powered Trajectory Optimization for Resupply
- 3D Automated Anisotropic Metric-Based Mesh Adaption for Hypersonic Flow
Awards with the same topic code
Verified by an exact topic code match. This is not a text-similarity match.
- Detailed and Reduced Chemical Kinetic Model Development for Rocket Hydrocarbon Combustion
- Shock-Tube-Validated, Versatile Kinetic Mechanism Reduction Framework for Mixed Hydrocarbon-Based Rocket Fuels
- Detailed and Reduced Chemical Kinetic Model Development for Rocket Hydrocarbon Combustion
- Development of Reduced Chemical Kinetic Models for Hydrocarbon Fuels Validated by High-Pressure Flow Reactor Experiments
Research funding history
125 SBIR/STTR records share this UEI (2002–2025). Reported award amounts total $58,455,367. 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