Pioneer Astronautics has developed a system that harvests CO2 from a simulated Martian atmosphere and reacts it with H2 into rocket propellant at a rate of 1 kg/day. A prototype system operated autonomously for 5 consecutive days, during which it maintained a 100% conversion rate (to detectable limits) of CO2 and H2 into products, maintaining a constant O2:CH4 ratio in the product stream with only minor adjustments. The integrated Mars in situ propellant production system (IMISPPS) uses a mixed catalyst bed to conduct the Sabatier methanation reaction and the reverse water gas shift in a single reactor. A recycle loop makes performance resistant to operational changes, with product ratios stable regardless of reactor temperature changes of as much as 100°C. An optimized IMISPPS is projected to produce 1 kg/day of O2:CH4 propellant and have a mass of 50 kg with a methane purity of 98+% while consuming 700 W of electrical power. With hydrogen from Earth, the system demonstrates a mass leverage of 18:1 in useful rocket propellant produced on Mars compared with imported feedstock.


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    Titel :

    Integrated Mars In Situ Propellant Production System


    Beteiligte:

    Erschienen in:

    Erscheinungsdatum :

    2012-12-15


    Format / Umfang :

    142013-01-01 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



    Integrated Mars In Situ Propellant Production System

    Zubrin, Robert M. | Online Contents | 2013


    Integrated Mars In Situ Propellant Production System

    Zubrin, Robert M. | Online Contents | 2013


    Integrated Mars In Situ Propellant Production System

    Zubrin, Robert M. | Online Contents | 2013


    In Situ Propellant Production on Mars

    Messina, Gabriele / Vasile, Massimiliano / Davighi, Andrea et al. | AIAA | 2005


    Investigation of Mars In-Situ Propellant Production

    MacKnight, Allen / Reddig, Mike | SAE Technical Papers | 1997