Experimental Study of the Lift Augmentation Potential Performance of Fluidic Propulsion for Advanced Air Mobility--The Upper Surface Blown Wing
Award amount
$149,337Program and phase
STTR · Phase IAward year
2021Award details
- Awarding agency
- Department of Defense
- Branch
- Air Force
- Recipient company
- JETOPTERA INC
- Proposal award date
- 2020-12-01
- Contract end date
- 2021-06-01
- UEI
- LYRYNP6K9VB1
- Solicitation number
- X20.D
- Topic code
- AFX20D-TCSO1
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.
- Wind Tunnel Experimental Evaluation of HEDWIG: A High-Speed Vertical Take-Off and Landing Blended Wing Body Aircraft powered by Fluidic Propulsion and Uppers Surface Blown Technology
- Fluidic Propulsive System: High Speed Vertical Take Off and Landing Propulsion for Project Hedwig Low Probability of Detection Aircraft
- Experimental Study of the Aerodynamic and Aeroacoustic Performance of Fluidic Propulsion for Advanced Air Mobility
Awards with the same topic code
Verified by an exact topic code match. This is not a text-similarity match.
- Extremely Lightweight and Ultra-Low Noise Isolated DC-DC Converters
- Continuous Fiber Additive Manufacturing for Rapid Prototyping and Demonstration of Small UAS Designs
- Deployable Containerized LH2 Refueling System
- Extremely Lightweight and Ultra-Low Noise Isolated DC-DC Converters
- Advanced Li-Metal, High-Power Battery
Research funding history
4 SBIR/STTR records share this UEI (2021–2022). Reported award amounts total $1,795,528. Reported amounts are not federal obligations.
Phases: Phase I, Phase II – Direct to Phase II, Phase II
Agencies: Department of Defense