SBIR/STTR Research Award
Design Of A High Performance External-Compression Inlet For Cruise At Mach 2.4
Award amount
$69,902Program and phase
SBIR · Phase IAward year
1997Award details
- Awarding agency
- National Aeronautics and Space Administration
- Branch
- Not reported
- Recipient company
- TechLand Research, Inc.
- Proposal award date
- Not reported
- Contract end date
- Not reported
- UEI
- FNKMWV5B2C96
- Solicitation number
- Not reported
- Topic code
- Not reported
Research abstract
N/A
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.
- Innovative Methods for Parametric Bleed Pattern Variation in Wind Tunnel Models
- Innovative Methods for Parametric Bleed Pattern Variation in Wind Tunnel Models
- Design of a Highly Compact Supersonic Cruise Missile (SSCM) Inlet
- Mode Transition Variable Geometry for High Speed Inlets for Hypersonic Aircraft
- Airflow Controller and Isolator for Pulse Detonation Engines
Research funding history
12 SBIR/STTR records share this UEI (1997–2017). Reported award amounts total $2,464,929. Reported amounts are not federal obligations.
Phases: Phase I, Phase II
Agencies: National Aeronautics and Space Administration, Department of Defense