Small Business Innovation Research/Small Business Tech Transfer
High Regression Rate, High Density Hybrid Fuels, Phase I
Project Introduction
This SBIR program will investigate high energy density novel nanofuels combined with high density binders for use with an N2O oxidizer. Terves has developed processes for stabilizing advanced high Isp fuels, such as LiBH4 to make them stable in thermoplastic binders such as PE. If they combust efficiently and have suitable regression rates and stability, These materials can provide hybrid Isp's above 300 and density Isp's above 450 seconds with self-pressurizing N2O oxidizers, enabling very low cost propulsion systems to be designed. This program will fabricate ultrafine- and nano- metal boride and hydride fuels, disperse them into high density binders, and evaluate their combustion efficiency in a hybrid test motor
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Anticipated Benefits
Hybrid rocket motors offer potential for reducing the cost and weight of propulsion systems. Higher efficiency, and higher regression rate solid fuels can be leveraged into revolutionary system performance for a variety of missions from mars sample return to upper stage and micro-satellite propulsion. Commercial applications are rapidly increasing with a reduction in the cost of access to space. N2O self-pressurizing Hybrid motors are viable low cost alternatives, as evidenced by their selection and use in spaceship one.
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Primary U.S. Work Locations and Key Partners
| Organizations Performing Work | Role | Type | Location |
|---|---|---|---|
| Terves Inc. | Lead Organization | Industry | Euclid, Ohio |
Jet Propulsion Laboratory
(JPL)
|
Supporting Organization | NASA Center | Pasadena, California |
Primary U.S. Work Locations
-
California
-
Ohio
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Organizational Responsibility
Responsible Mission Directorate:
- Space Technology Mission Directorate (STMD)
Lead Organization:
- Terves Inc.
Responsible Program:
- Small Business Innovation Research/Small Business Tech Transfer
Project Management
Program Director:
Program Manager:
Principal Investigator:
Project Duration
Start: Jun 2014
End: Dec 2014
Technology Maturity (TRL)
| Start: | 3 |
| Current: | 4 |
| Estimated End: | 4 |
Applied Research
Development
Demo & Test
Technology Areas
Primary:
- TX01 Propulsion Systems
- TX01.1 Chemical Space Propulsion
- TX01.1.5 Hybrids
Target Destination
Earth
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