Mission operations are presented for comet rendezvous and outer planet exploration NEP spacecraft employing in-core thermionic reactors for electric power generation. The selected reference missions are the Comet Halley rendezvous and a Jupiter orbiter at 5.9 planet radii, the orbit of the moon Io. The characteristics of the baseline multi-mission NEP spacecraft are presented and its performance in other outer planet missions, such as Saturn and Uranus orbiters and a Neptune flyby, are discussed. Candidate mission operations are defined from spacecraft assembly to mission completion. Pre-launch operations are identified. Shuttle launch and subsequent injection to earth escape by the Centaur D-1T are discussed, as well as power plant startup and the heliocentric mission phases. The sequence and type of operations are basically identical for all missions investigated.


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    Titel :

    Mission operations for unmanned nuclear electric propulsion outer planet exploration with a thermionic reactor spacecraft.


    Beteiligte:
    Spera, R. J. (Autor:in) / Prickett, W. Z. (Autor:in) / Garate, J. A. (Autor:in) / Firth, W. L. (Autor:in)

    Kongress:

    Annual Thermionic Conversion Specialist Conference ; 1971 ; San Diego, CA


    Erscheinungsdatum :

    1971-01-01


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :