The SERT D (Space Electric Rocket Test - D) study defines a possible spacecraft project that would demonstrate the use of electric ion thrusters for long-term (5 yr) station keeping and attitude control of a synchronous orbit satellite. Other mission objectives included in the study were: station walking to satellite rendezvous and inspection, use of low cost attitude sensing system, use of an advanced solar array orientation and slip ring system, and an ion thruster integrated directly with a solar array power source. The SERT D spacecraft, if launched, will become SERT 3 the third space electric thruster test.


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    Titel :

    SERT D spacecraft study


    Erscheinungsdatum :

    1974-01-01


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :



    Sert 2 Spacecraft Attitude Response

    B. E. Leroy / R. R. Lovell / J. D. Regetz | NTIS | 1971


    SERT 2 spacecraft attitude response

    Leroy, B. E. / Lovell, R. R. / Regetz, J. D. | NTRS | 1971


    SERT 2 spacecraft electrical power system

    Krawczyk, R. J. | NTRS | 1971


    Design of SERT 2 spacecraft structures

    Sharp, G. R. | NTRS | 1971