Steady state tests of the thruster 2 system on the SERT 2 spacecraft are presented. A direct thrust measurement was obtained for the ion thruster during operations to increase the spacecraft spin rate to maintain spacecraft attitude stability. The continued restart tests of thruster 1 and a report on the general status of all spacecraft systems including the main solar array are presented.


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    Titel :

    Sert 2 1979 Extended Flight Thruster System Performance


    Beteiligte:
    W. R. Kerslake (Autor:in) / L. R. Ignaczak (Autor:in)

    Erscheinungsdatum :

    1979


    Format / Umfang :

    22 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch





    SERT II 1979 extended flight thruster system performance

    Kerslake, W. R. / Ignaczak, L. R. | NTRS | 1979


    SERT II 1979 extended flight thruster system performance

    KERSLAKE, W. / IGNACZAK, L. | AIAA | 1979


    SERT 2 1979 extended flight thruster system performance

    Kerslake, W. R. / Ignaczak, L. R. | NTRS | 1979


    SERT II 1980 extended flight thruster experiments

    KERSLAKE, W. / IGNACZAK, L. | AIAA | 1981