Propulsion integration for low-cost, extended-range, attritable UAS
Award amount
$1,486,090Program and phase
SBIR · Phase IIAward year
2020Award details
- Awarding agency
- Department of Defense
- Branch
- Air Force
- Recipient company
- EMPIRICAL SYSTEMS AEROSPACE INC
- Proposal award date
- 2020-02-25
- Contract end date
- 2022-02-25
- UEI
- MFCTLU3MRXC8
- Solicitation number
- N/A
- Topic code
- A2.10
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.
- Hydrogen Propulsion Energy (HyPE) Module for Aircraft Sizing and Analysis
- Apprehension of High-altitude Aircraft and Balloons (AHAB)
- ESA-ALE: Electric Small Aircraft – Air Launch Effect via Valkyrie
- Aircraft Traction Inverter for Hybrid-Electric and All-Electric Megawatt-Class Vehicles
- Wind Tunnel and Flight Testing of Scalable Modular Aerial Research Testbed
Awards with the same topic code
Verified by an exact topic code match. This is not a text-similarity match.
- Extension of the Eddy Dissipation Concept for Improved Low-Cost Turbulence-Chemistry Interaction Modeling
- Skin Friction and Pressure Measurements in Supersonic Inlets
- Microtextured Surfaces for Turbine Blade Impingement Cooling
- Coupled Transpired and Discretely Injected Films
- Development of Axial Compressor Heat-Extraction Capability for Thermal Management Applications
Research funding history
37 SBIR/STTR records share this UEI (2009–2024). Reported award amounts total $15,614,972. Reported amounts are not federal obligations.
Phases: Phase I, Phase II, Phase II – Direct to Phase II
Agencies: National Aeronautics and Space Administration, Department of Defense