SBIR/STTR Research Award
A MULTI-FIDELITY SUPERSONIC FLOW SOLVER FOR PRELIMINARY DESIGN & OPTIMIZATION
Award amount
$1,248,744Program and phase
SBIR · Phase II – Direct to Phase IIAward year
2023Award details
- Awarding agency
- Department of Defense
- Branch
- Air Force
- Recipient company
- RESEARCH IN FLIGHT LLC
- Proposal award date
- 2023-02-10
- Contract end date
- 2024-11-10
- UEI
- NN8QT8JVKRH5
- Solicitation number
- X23.4
- Topic code
- AFX234-DCSO2
Research abstract
Research in Flight and Utah State University are proposing the development of an early-design simulation capability for transonic, supersonic and hypersonic flight vehicles. This capability will address the emerging requirements of U.S. Air Force customer
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.
- Performance and Acoustic Design Optimization Tools for Cyclonic Vortex Engines
- A Rapid Aerodynamic Prediction Tool for Maneuvering Hypersonic Air Vehicles
- Accelerated preconditioned RANS simulations for Hypersonic Flight Vehicles
- Real-Time Assessment of Battle Damage on Air Vehicle Mission Profiles
- A Rapid Aerodynamic Prediction Tool for Maneuvering Hypersonic Air Vehicles
Awards with the same topic code
Verified by an exact topic code match. This is not a text-similarity match.
- AeroISU: Real-time Visibility and Mission Readiness of Industrial Storage Units (ISU), Containers & other USAF Equipment
- Trans Astronautica’s Sutter Turn Key Observatory
- Quantum Secure Identification
- Low-Probability-of-Intercept Terahertz Communications for Air Force Applications
- Accrete Argonaut Sequential
Research funding history
17 SBIR/STTR records share this UEI (2015–2024). Reported award amounts total $6,523,990. 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