Energetic Ion Mitigation Methodology for High Power Plasma Thruster Cathodes
Award amount
$199,725Program and phase
SBIR · Phase IAward year
2013Award details
- Awarding agency
- National Aeronautics and Space Administration
- Branch
- Not reported
- Recipient company
- Electrodynamic Applications Inc
- Proposal award date
- 2013-05-23
- Contract end date
- 2013-11-23
- UEI
- EKN4D4FDZNV9
- Solicitation number
- Not reported
- Topic code
- E1.01
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.
- Integrated Energetic Ion Mitigation for High Power Plasma Cathodes
- Divergent Field Annular Ion Engine
- Fiber-Optic Pyrometer for Thermal Protection Systems
- Nonintrusive fiber interferometer for ablative TPS recession measurement
- Hybrid Chemical-Electric Propulsion (HCEP)
Awards with the same topic code
Verified by an exact topic code match. This is not a text-similarity match.
- 300C/15 kW power converter with AlGaN/GaN-Si MOS-HFETs for electric propulsion systems
- Hall Effect Thruster for High Power Solar Electric Propulsion Technology Demonstration
- Hall Effect Thruster for High Power Solar Electric Propulsion Technology Demonstration
- High Input Voltage Hall Thruster Discharge Converter
- Direct Drive Unit with Autonomous Cathode Current Regulation
Research funding history
29 SBIR/STTR records share this UEI (2003–2015). Reported award amounts total $7,439,985. Reported amounts are not federal obligations.
Phases: Phase I, Phase II
Agencies: Department of Defense, National Aeronautics and Space Administration, National Science Foundation