Pluto Orbiter/lander and sample return missions are not impossible using chemical propulsion, but are possible with nuclear thermal propulsion. Using the MITEE nuclear engine, a spacecraft could first orbit Pluto, mapping it, and then land at a selected site, 12 years after the departure form Earth. If surface water/ice is available, fresh H/sub 2/ propellant could be manufactured by electrolysis of melt H/sub 2/O using power from the bi-modal nuclear engine, enabling multiple hops to new sites for further data collection. A warm water probe could also be deployed to explore the interior of Pluto's ice sheets. After completing exploration, the spacecraft could return samples from Pluto to Earth with a 12-year trip time. Mission architectures and the design of the spacecraft, nuclear propulsion engine, propellant manufacturing unit and warm water probe are described herein.


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    Titel :

    Pluto Orbiter/lander/sample return missions using the MITEE nuclear engine


    Beteiligte:
    Powell, J. (Autor:in) / Maise, G. (Autor:in) / Paniagua, J. (Autor:in)


    Erscheinungsdatum :

    01.01.2003


    Format / Umfang :

    1793511 byte





    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



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