SBIR/STTR
Hybrid Propulsion for Upper-Stage Boosters, Phase II
Project Introduction
The objective of the proposed research and development effort is to demonstrate the feasibility of an innovative approach to high-performance hybrid propulsion for upper-stages. The missions for these propulsion systems include launching small- and nano-satellites and conducting hypersonic flight test operations. The focus of the research effort will be on achieving high specific impulse by means of an innovative approach to nozzle design. The technology will be experimentally demonstrated in a series of hot-fire tests during the proposed research program.
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Anticipated Benefits
Potential NASA Commercial Applications: Small and nano-satellite launchers, Hypersonic flight test for propulsion and materials development, sub-orbital sounding rockets.
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Primary U.S. Work Locations and Key Partners
| Organizations Performing Work | Role | Type | Location |
|---|---|---|---|
Armstrong Flight Research Center
(AFRC)
|
Lead Organization | NASA Center | Edwards, CA |
| Exquadrum, Inc. | Supporting Organization | Industry | Adelanto, CA |
| University of Alabama at Hunstville | Supporting Organization | Academic | Huntsville, AL |
Primary U.S. Work Locations
-
Alabama
-
California
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Organizational Responsibility
Responsible Mission Directorate:
- Space Technology Mission Directorate (STMD)
Lead Center / Facility:
- Armstrong Flight Research Center (AFRC)
Responsible Program:
- SBIR/STTR
Project Management
Program Director:
Program Manager:
Project Manager:
Principal Investigator:
- Kevin E Mahaffy
Project Duration
Start: Jul 2013
End: Sep 2015
Technology Maturity (TRL)
| Start: | 4 |
| Current: | 5 |
| Estimated End: | 5 |
Applied Research
Development
Demo & Test
Technology Areas
Primary:
- TA 2 In-Space Propulsion Technologies
- TA 2.1 Chemical Propulsion
- TA 2.1.5 Hybrid
Other / Cross-cutting:
- TA 1 Launch Propulsion Systems
- TA 1.5 Unconventional and Other Propulsion Systems
- TA 1.5.2 Air Launch and Drop Systems