High Speed Closed Brayton Cycle Turboalternator
Award amount
$124,776Program and phase
SBIR · Phase IAward year
2016Award details
- Awarding agency
- National Aeronautics and Space Administration
- Branch
- Not reported
- Recipient company
- MOHAWK INNOVATIVE TECHNOLOGY, INC.
- Proposal award date
- 2016-06-10
- Contract end date
- 2016-12-09
- UEI
- ZY3GYFN4ELC4
- Solicitation number
- Not reported
- Topic code
- H8.01
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.
- Configurable Array of 3D-Printed Lubrication-Free Turbocompressors for High Temperature Industrial Heat Pump Applications
- Additively Manufactured High Temperature Centrifugal Impellers for Low Cost SOFC Recycle Blower
- 3D-Printed Compressor-Turbine Sets with Internal Cooling
- Innovative Turbine Engine Propulsion Solutions for Class 3 Unmanned Aerial Vehicles
- High Speed Closed Brayton Cycle Turboalternator
Awards with the same topic code
Verified by an exact topic code match. This is not a text-similarity match.
- Membrane-Supported Thermoelectric Generator
- Liquid Interface Diffusion Bonding of FPS Heat Pipes to Core
- High Speed Data Capability to Increase the Utilization of the Materials International Space Station Experiment (MISSE-FF) Flight Facility
- Evaluation of Multifunctional Radiation Shielding Material Against Long Duration Space Environment - Utilization of MISSE-FF
- Microgravity Granular Material Research (MGMR) Facility for ISS
Research funding history
105 SBIR/STTR records share this UEI (1995–2022). Reported award amounts total $40,033,528. Reported amounts are not federal obligations.
Phases: Phase I, Phase II, Phase II – Direct to Phase II
Agencies: Department of Defense, Department of Energy, National Aeronautics and Space Administration, Department of Health and Human Services, National Science Foundation, Department of Commerce