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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    Titel :

    Advanced propulsion for the Mars Rover Sample Return Mission


    Beteiligte:

    Erscheinungsdatum :

    1988-07-01


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Advanced propulsion for the Mars Rover Sample Return Mission

    PALASZEWSKI, BRYAN / FRISBEE, ROBERT | AIAA | 1988



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    Mars Rover Sample Return mission

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    Mars Rover Sample Return mission study

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