Small Business Innovation Research/Small Business Tech Transfer
High-Performance, Pump-Fed Propulsion for Mars Ascent Vehicle Applications
Project Description
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 optimizing a MON-30 electric pump previously built under an earlier NASA SBIR to offer further efficiency improvements, and to provide a competitive liquid bipropellant propulsion system as an alternative to the existing solid / hybrid propellant designs for a Mars Ascent Vehicle.
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Anticipated Benefits
While the proposed pump-fed propulsion system has direct applications for Mars Ascent Vehicles and sample return missions, the enabling technology proposed herein overcomes a key challenge of providing on-board pressurization at the small-scale, thereby enabling a new generation liquid bipropellant rocket engines in the 100-5,000lbf thrust class, with a T/W ratio in excess of 100, and a vacuum Isp >300sec. Other NASA applications for such high-performance propulsion systems are therefore also likely to include lunar ascent / descent missions (precursor rovers, cargo, etc.), Near-Earth-Object (NEO) missions and outer planet orbit capture and insertion.
Beyond NASA applications, the proposed high-performance pumps are expected to have wide relevance to upper stage propulsion technology for small commercial launch vehicles, advanced Department of Defense vehicles such as XS-1, commercial lander missions, orbit insertion engines for commercial satellites, and apogee kick motors for orbit circularization of commercial satellites. More »
Beyond NASA applications, the proposed high-performance pumps are expected to have wide relevance to upper stage propulsion technology for small commercial launch vehicles, advanced Department of Defense vehicles such as XS-1, commercial lander missions, orbit insertion engines for commercial satellites, and apogee kick motors for orbit circularization of commercial satellites. More »
Project Library
Primary U.S. Work Locations and Key Partners
| Organizations Performing Work | Role | Type | Location |
|---|---|---|---|
| Astra Space, Inc | Lead Organization | Industry | Louisville, Colorado |
| Jet Propulsion Laboratory (JPL) | Supporting Organization | FFRDC/UARC | Pasadena, California |
Primary U.S. Work Locations
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California
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