The principle objective of Phase 2 was to produce an engineering model N2H4 arcjet system which met typical performance, lifetime, environmental, and interface specifications required to support a 10-year N-S stationkeeping mission for a communications spacecraft. The system includes an N2H4 arcjet thruster, power conditioning unit (PCU), and the interconnecting power cable assembly. This objective was met with the successful conclusion of an extensive system test series.


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    Titel :

    Arcjet thruster research and technology, phase 2


    Beteiligte:
    Yano, Steve E. (Autor:in)

    Erscheinungsdatum :

    1991-03-01


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Arcjet thruster research and technology

    Makel, Darby B. / Cann, Gordon L. | NTRS | 1988


    Arcjet thruster development

    Auweter-Kurtz, M. / Glocker, B. / Goelz, T. et al. | AIAA | 1996


    Arcjet Thruster Development

    Auweter-Kurtz, M. | Online Contents | 1996


    Medium power arcjet thruster experiments

    GLOCKER, BERND / AUWETER-KURTZ, MONIKA / GOELZ, THOMAS et al. | AIAA | 1990


    Plume characteristics of an arcjet thruster

    LIEBESKIND, JOHN / HANSON, RONALD / CAPPELLI, MARK | AIAA | 1993