Comparison is made of chemical, nuclear heat transfer, and electrical propulsion systems for Mars missions selecting probe, Mars orbiters, and soft-landing mission as best typifying energy requirements; data relative to booster capabilities and mission outline, analysis of power plants, method of obtaining energy requirements, and payload data for various boosters and upper-stage propulsion units; trajectory considerations; results presented.


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    Titel :

    What kind of upper-stage propulsion for mars missions


    Weitere Titelangaben:

    Astronautics Aerospace Eng


    Beteiligte:
    Cohen, A.D. (Autor:in) / Beers, L.S. (Autor:in)


    Erscheinungsdatum :

    1963


    Format / Umfang :

    8 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Aerobraking in Advanced Propulsion Mars Missions

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    Mars Missions Using Solar Electric Propulsion

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    Propulsion needs for lunar/Mars missions

    Woodcock, Gordon R. | NTRS | 1990