A Mars ascent propulsion system trade study was conducted to determine 1) what propulsion technologies allow a Mars sample return mission to be launched on a Delta III class launch verhicle, and 2) whether more exotic technologies, such as in-situ propellant production, allow major cost savings by enabling the use of a smaller launch vehicle or a direct return from the Martian surface to Earth without the need of a rendezvous in the Martian orbit.


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    Titel :

    Evaluation of Some Candidate Propulsion Technologies for Mars Ascent Vehicle


    Beteiligte:
    Guernsey, C. S. (Autor:in) / Thunnissen, D. P. (Autor:in) / Adler, M. (Autor:in) / French, J. R. (Autor:in)

    Erscheinungsdatum :

    12.01.1998


    Medientyp :

    Preprint


    Format :

    Keine Angabe


    Sprache :

    Englisch




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