Ion propulsion modules employing 8 cm thrusters and 30 cm thrusters were studied for Multimission Modular Spacecraft (MMS) applications. Recurring and non-recurring cost elements were generated for these modules. As a result, ion propulsion cost drivers were identified to be Shuttle charges, solar array, power processing, and thruster costs. Cost effective design approaches included short length module configurations, array power sharing, operation at reduced thruster input power (reduced solar array size), simplified power processing units, and power processor output switching.


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    Titel :

    Ion propulsion cost effectivity


    Beteiligte:
    Zafran, S. (Autor:in) / Biess, J. J. (Autor:in) / Callens, R. A. (Autor:in)

    Kongress:

    International Electric Propulsion Conference ; 1979 ; Princeton, NJ


    Erscheinungsdatum :

    1979-10-01


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch




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    ZAFRAN, S. / BIESS, J. / CALLENS, R. | AIAA | 1979


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    Zafran, S. / Biess, J. J. | NTRS | 1978


    Ion propulsion cost effectivity

    Zafran, S. / Bless, J.J. / Callens, R.A. | Tema Archiv | 1979


    Ion Propulsion Cost Effectivity

    S. Zafran / J. J. Biess | NTIS | 1978


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