The results are presented of an investigation of the factors which affect the determination of Spacelab (S/L) minimum interface main dc voltage and available power from the orbiter. The dedicated fuel cell mode of powering the S/L is examined along with the minimum S/L interface voltage and available power using the predicted fuel cell power plant performance curves. The values obtained are slightly lower than current estimates and represent a more marginal operating condition than previously estimated.


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    Titel :

    Space shuttle engineering and operations support. Orbiter to spacelab electrical power interface. Avionics system engineering


    Beteiligte:
    Emmons, T. E. (Autor:in)

    Erscheinungsdatum :

    30.06.1976


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Space shuttle engineering and operations support. Avionics system engineering

    Broome, P. A. / Neubaur, R. J. / Welsh, R. T. | NTRS | 1976


    Space Shuttle Engineering and Operations Support. Avionics System Engineering

    P. A. Broome / R. J. Neubaur / R. T. Welsh | NTIS | 1976


    Space shuttle orbiter avionics

    Carrier, L.M. / Minor, R.G. | Tema Archiv | 1977


    Space Shuttle orbiter avionics

    CARRIER, L. / MINOR, R. | AIAA | 1977