OpenVSP Smart Conceptual Design Tool Improvements, Including Inboard Profile Visualization
Award amount
$149,994Program and phase
SBIR · Phase IAward year
2014Award details
- Awarding agency
- Department of Defense
- Branch
- Air Force
- Recipient company
- EMPIRICAL SYSTEMS AEROSPACE INC
- Proposal award date
- 2014-05-07
- Contract end date
- 2015-02-09
- UEI
- MFCTLU3MRXC8
- Solicitation number
- 2014.1
- Topic code
- AF141-083
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.
- Smart Aircraft Conceptual Design in Multidisplinary Design Optimization
- Smart Aircraft Conceptual Design in Multidisplinary Design Optimization
- 3-D Smart Aircraft Conceptual Design Tool
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