The present evaluation of highly detailed advanced propulsion system design concepts for the Mars Rover Sample Return Mission proceeded by comparing a baseline chemical propulsion option with both storable and cryogenic advanced chemical propulsion alternatives and solar- and nuclear-based electric propulsion OTVs. Substantial launch mass reductions and commensurate payload mass increases were obtainable with both advanced chemical and electric propulsion cycles.


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    Title :

    Advanced propulsion for the Mars Rover Sample Return Mission


    Contributors:

    Publication date :

    1988-07-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English




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