Electric propulsion promises the advantage of providing high Isp's for placing payloads into their assigned orbits. This translates into heavier payloads using a given lift capability or, conversely, the use of smaller boosters. To accomplish this, high electric powers are required. Space reactor power systems such as SP-100 enable this technology. The electric propulsion requirements needed, namely, their power requirements and the resulting payload masses and time-to-orbit, are shown. Also indicated are the missions most benefitting from the use of electric propulsion. An Interim Reference Mission is described, synthesizing the results shown, for demonstration purposes.


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    Titel :

    Electric propulsion applications enabled by space nuclear power


    Beteiligte:
    Vicente, F. A. (Autor:in) / Karras, T. (Autor:in) / Brewer, L. (Autor:in) / Gore, R. (Autor:in)

    Erscheinungsdatum :

    01.07.1989


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Electric propulsion applications enabled by space nuclear power

    VICENTE, F. / KARRAS, T. / BREWER, L. et al. | AIAA | 1989


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    Vicente, F. A. / Karras, T. / Darooka, D. et al. | NTRS | 1989


    Space nuclear power applied to electric propulsion

    Vicente, F.A. / Karras, T. / Darooka, D. et al. | Tema Archiv | 1989



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