The results of a current study program to develop a rational basis for selection of power processing, distribution, and control configurations for future aerospace vehicles including the Space Station, Space Shuttle, and high-performance aircraft are presented. Within the constraints imposed by the characteristics of power generation subsystems and the load utilization equipment requirements, the power processing, distribution and control subsystem can be optimized by selection of the proper distribution voltage, frequency, and overload/fault protection method. It is shown that, for large space vehicles which rely on static energy conversion to provide electric power, high-voltage dc distribution (above 100 V dc) is preferable to conventional 28 V dc and 115 V ac distribution per MIL-STD-704A. High-voltage dc also has advantages over conventional constant frequency ac systems in many aircraft applications due to the elimination of speed control, wave shaping, and synchronization equipment.


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    Titel :

    Electric power processing, distribution and control for advanced aerospace vehicles.


    Beteiligte:
    Krausz, A. (Autor:in) / Felch, J. L. (Autor:in)

    Kongress:

    Power Processing and Electronics Specialists Conference ; 1972 ; Atlantic City, NJ


    Erscheinungsdatum :

    01.01.1972


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Advanced aerospace power distribution and control techniques.

    Jeffcoat, T. D. / Eastman, F. E. | NTRS | 1972


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    Johnson, R. L. / Manganiello, E. J. | NTRS | 1970


    Aerospace Lubrication for Advanced Vehicles

    R. L. Johnson / E. J. Manganiello | NTIS | 1970


    Aerospace lubrication for advanced vehicles

    Johnson, R. L. / Manganiello, E. J. | NTRS | 1970