SBIR/STTR Research Award
Plume Induced Missile Body Heating
Award amount
$69,970Program and phase
SBIR · Phase IAward year
2003Award details
- Awarding agency
- Department of Defense
- Branch
- Missile Defense Agency
- Recipient company
- COMBUSTION RESEARCH & FLOW TECHNOLOGY INC
- Proposal award date
- Not reported
- Contract end date
- Not reported
- UEI
- XGYZK5MHNJZ8
- Solicitation number
- Not reported
- Topic code
- Not reported
Research abstract
The innovation for this Phase I program is the performance of a scope-out study that quantifies missile body heating effects due to plume interactions in the continuum altitude range of 30-80 km where plume induced separation is significant. The size andcharacteristics of the separation zone at altitudes of 30-60 km are largely controlled by turbulent transitional behavior and an advanced
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
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