The Space Shuttle Orbiter Auxiliary Power Unit subsystem has operated successfully on three vehicles by meeting mission requirements and has proven the design for space operation. The current Auxiliary Power Unit (APU) operational life is limited to 12 missions and the APU turnaround between flights is longer than originally anticipated. The Improved APU objective is to increase life to 50 missions, reduce the three - APU subsystem vehicle weight by 140 lbs., and reduce turnaround time. The design changes incorporated into the Improved APU and the associated development testing are described.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Space Shuttle Orbiter improved auxiliary power unit


    Beteiligte:
    Hagemann, D. W. (Autor:in) / Wicklund, L. L. (Autor:in) / Loken, G. R. (Autor:in) / Baughman, J. R. (Autor:in) / Lance, R. J. (Autor:in)


    Erscheinungsdatum :

    01.02.1984


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Space Shuttle Orbiter Auxiliary Power Unit

    Weary, D. / Baughman, J. / Wicklund, L. et al. | SAE Technical Papers | 1982


    Space Shuttle Orbiter auxiliary power unit

    Mckenna, R. / Wicklund, L. / Baughman, J. et al. | NTRS | 1982


    Space Shuttle Orbiter auxiliary power unit status

    Reck, M. / Loken, G. / Horton, J. et al. | NTRS | 1991


    Space Shuttle Orbiter Auxiliary Power Unit Status

    Loken, G. / Baughman, J. / Horton, J. et al. | SAE Technical Papers | 1991