The requirements imposed on the airbreathing engines by the shuttle mission and some results from engine design studies are discussed. In particular, some of the engine system weight study results are presented, potential problem areas and required engine modifications are identified, and testing requirements for a development and qualification program are discussed. The engines of interest for the shuttle are engines that are currently being developed for other applicatons. The potential problems, engine modifications, and testing requirements result primarily from the new environments associated with launch, space residence, and reentry.


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    Titel :

    Airbreathing engines for space shuttle


    Beteiligte:
    Glassman, A. J. (Autor:in) / Stewart, W. L. (Autor:in) / Nosek, S. M. (Autor:in)

    Kongress:

    Natl. Aerospace Eng. and Manuf. Meeting ; 1972 ; San Diego, CA, United States


    Erscheinungsdatum :

    01.01.1972


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Airbreathing Engines for Space Shuttle

    Glassman, Arthur J. / Nosek, Stanley M. / Stewart, Warner L. | SAE Technical Papers | 1972


    Shuttle airbreathing propulsion

    GLASSMAN, A. / NOSEK, S. | AIAA | 1971



    Space shuttle airbreathing engine exhaust effects

    Ehrlich, C. F., Jr. | NTRS | 1970


    Shuttle Airbreathing Propulsion

    A. J. Glassman / S. M. Nosek / W. L. Stewart | NTIS | 1971