Mars Integrated Propellant Production System

Award Information
Agency:
National Aeronautics and Space Administration
Branch
n/a
Amount:
$69,941.00
Award Year:
2005
Program:
SBIR
Phase:
Phase I
Contract:
NNK05OA25C
Agency Tracking Number:
040452
Solicitation Year:
2004
Solicitation Topic Code:
X1.03
Solicitation Number:
n/a
Small Business Information
Pioneer Astronautics
11111 W. 8th Ave., Unit A, Lakewood, CO, 80215-5516
Hubzone Owned:
N
Socially and Economically Disadvantaged:
N
Woman Owned:
N
Duns:
120561456
Principal Investigator:
Anthony Muscatello
Principal Investigator
(303) 980-0759
tony.muscatello@pioneerastro.com
Business Contact:
Robert Zubrin
Business Official
(303) 980-0890
zubrin@aol.com
Research Institution:
n/a
Abstract
The Integrated Mars In-Situ Propellant Production System (IMISPPS) is an end-to-end system that will produce rocket propellant on Mars from CO2 in the Martian atmosphere. The IMISPPS combines the RWGS and Sabatier reactions in a single reactor to produce a useful high-specific impulse fuel (methane plus carbon monoxide) and water, which is condensed and electrolyzed to produce oxygen and hydrogen. The hydrogen is recycled back to the Sabatier/RWGS reactor to react with Martian CO2 to produce more fuel, while the oxygen is cryogenically stored to provide oxidizer. Some of the carbon monoxide is removed by cryogenic separation to increase propellant specific impulse. Carbon dioxide acquisition to feed the fuel reactor is accomplished using a lightweight freezer. Use of the IMISPPS has the advantage of producing all the oxygen needed to burn the methane with only in a single catalytic reactor required. In the proposed work, we will build a brassboard core of the IMSIPPS and demonstrate its performance and reliability.

* information listed above is at the time of submission.

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