SBIR/STTR
On-Board Pressurization Systems for Sample Return Missions, Phase I
Project Introduction
To-date, the realization of high-performance liquid bipropellant rocket engines for ascent vehicle and sample return applications has largely been hindered by the inability to obtain "on-board" pressurization through a light-weight and low-complexity pump. Ventions seeks to fulfill this critical need by designing, fabricating and testing an electric pump for a Mars Ascent Vehicle compatible with LOX / propane produced via in-situ resource utilization to achieve significant performance improvements over the current baseline.
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Primary U.S. Work Locations and Key Partners
| Organizations Performing Work | Role | Type | Location |
|---|---|---|---|
| Ventions, LLC | Lead Organization | Industry | San Francisco, California |
Jet Propulsion Laboratory
(JPL)
|
Supporting Organization | NASA Center | Pasadena, California |
Primary U.S. Work Locations
-
California
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Organizational Responsibility
Responsible Mission Directorate:
- Space Technology Mission Directorate (STMD)
Lead Organization:
- Ventions, LLC
Responsible Program:
- SBIR/STTR
Project Management
Program Director:
Program Manager:
Principal Investigator:
Project Duration
Start: Jun 2014
End: Dec 2014
Technology Maturity (TRL)
| Start: | 3 |
| Current: | 3 |
| Estimated End: | 4 |
Applied Research
Development
Demo & Test
Technology Areas
Primary:
- TX01 Propulsion Systems
- TX01.1 Chemical Space Propulsion
- TX01.1.3 Cryogenic
Target Destinations
The Sun, Earth, The Moon, Others Inside the Solar System, Outside the Solar System, Mars
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