Studies by NASA have shown that many of the space missions proposed for the time period 1980 to 2000 will require large spacecraft structures to be assembled in orbit. Large antennas and power systems up to 2.5 MW size are predicted to supply the electrical/electronic subsystems, solar electric subsystems, solar electric propulsion, and space processing for the near-term programs. Platforms of 100 meters/length for stable foundations, utility stations, and supports for these multi-antenna and electronic powered mechanisms are also being considered. This paper includes the findings of an analytic and conceptual design study for large spacecraft power distribution, and electrical loads and their influence on the cable and connector requirements for these proposed large spacecraft.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    High voltage cabling for high power spacecraft


    Beteiligte:
    Dunbar, W. G. (Autor:in)

    Kongress:

    In: NAECON 1981 ; 1981 ; Dayton, OH


    Erscheinungsdatum :

    1981-01-01


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Spacecraft cabling for minimum magnetic moment

    Herring, T.H. | Tema Archiv | 1979


    Safety Modeling of High Voltage Cabling in Electrified Powertrains

    Marpu, Amar / Garfinkel, George / Maguire, Patrick | SAE Technical Papers | 2017


    Arc Suppression Coatings for Electrodynamic Tethers and Spacecraft Cabling

    Bilen, S. / Gilchrist, B. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2009


    Spacecraft high-voltage power supply construction

    Sutton, J. F. / Stern, J. E. | NTRS | 1975


    Spacecraft high-voltage power supply construction

    Sutton, John F. / Stern, Jesse E. | TIBKAT | 1975