The development of small sized, low weight spacecraft should lead to reduced scientific mission costs by lowering fabrication and launch costs. An order of magnitude reduction in spacecraft size can be obtained by miniaturizing components. Additional reductions in spacecraft weight, size, and cost can be obtained by utilizing the synergy that exists between different spacecraft systems. The state-of-the-art of three major systems, spacecraft power, propulsion, and communications is discussed. Potential strategies to exploit the synergy between these systems and/or the payload are identified. Benefits of several of these synergies are discussed.


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    Titel :

    Power, Propulsion, and Communications for Microspacecraft Missions


    Beteiligte:
    deGroot, W. A. (Autor:in) / Maloney, T. M. (Autor:in) / Vanderaar, M. J. (Autor:in)

    Kongress:

    Scientific Microsatellites ; 1997 ; Tainan, Taiwan, Province of China


    Erscheinungsdatum :

    01.03.1998


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Power, Propulsion and Communications for Microspacecraft Missions

    de Groot, W. A. / Maloney, T. M. / Vanderaar, M. J. et al. | British Library Conference Proceedings | 1999


    Power, Propulsion, and Communications for Microspacecraft Missions

    W. A. deGroot / T. M. Maloney / M. J. Vanderaar | NTIS | 1998


    Microspacecraft missions and systems

    Jones, Ross M. | NTRS | 1989


    Enabling technologies for microspacecraft missions

    Chun, Wendell / Gillespie, Timothy / Gamber, Terry | AIAA | 1999


    Planetary missions using microspacecraft technology

    Short, Kendra L. / Jones, Ross M. / Salvo, Christopher G. et al. | NTRS | 1992