Improved Hypersonic Jet Interaction Modeling with Propulsion Exhaust
Award amount
$1,495,396Program and phase
STTR · Phase IIAward year
2024Award details
- Awarding agency
- Department of Defense
- Branch
- Missile Defense Agency
- Recipient company
- COMBUSTION RESEARCH & FLOW TECHNOLOGY INC
- Proposal award date
- 2024-03-11
- Contract end date
- 2026-03-10
- UEI
- XGYZK5MHNJZ8
- Solicitation number
- 22.B
- Topic code
- MDA22-T005
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.
- Predicting RF Attenuation and Radar Cross Section Returns for High Fidelity 3D Missile Plumes and Hypersonic Wakes with Hardbody Interaction
- Efficient Models for Film Condensation in Cryogenic Tank Applications
- Framework for Transitioning DTRA High Fidelity Codes to APUs
- Landing Area and Rocket Plume Diagnostics
- A Multi-Zonal Multi-Timescale Modeling Framework to Accelerate Fluid-Thermal Analyses of Rotating Detonation Rocket Engines
Awards with the same topic code
Verified by an exact topic code match. This is not a text-similarity match.
- Reactive Jet Interactions with Multifidelity Turbulence and Tailored Multifidelity Combustion Modeling
- Reactive Jet Interactions with Multifidelity Turbulence and Tailored Finite-Rate Combustion Modeling
- Scalable Physics Modeling of Jet Interaction Phenomena
- Improved Hypersonic Jet Interaction Modeling with Propulsion Exhaust
- High-Resolution Modeling of Plume Exhaust Shock-Boundary Layer Interactions
Research funding history
303 SBIR/STTR records share this UEI (1995–2025). Reported award amounts total $121,181,328. 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