For interplanetary missions, highly efficient electric propulsion systems can be used to increase the mass delivered to the destination and/or reduce the trip time over typical chemical propulsion systems.


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    Titel :

    Preliminary Design of Low-Thrust Interplanetary Missions


    Beteiligte:
    Flanagan, S. (Autor:in) / Sims, J. (Autor:in)

    Erscheinungsdatum :

    16.08.1999


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch





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    J. A. Sims / S. N. Flanagan | NTIS | 1997


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    Compensator Design for Low-Thrust Interplanetary Missions

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