Technology problems relating to the shuttle thermal protection system and the auxiliary power units for flight control of engine gimbaling and aero surfaces are examined as well as yet unresolved difficulties associated with the main engine, external tank doors, and the payload bay doors. Concepts for launch crew escape and for flight inspection are discussed, and the orbital flight test drivers are identified. The majority of OFT objectives can be accomplished in a success oriented four flight program. Carry over will be accommodated in the operational phase with a mini-DFI package. Primary shuttle systems requiring additional testings are (1) aerodynamics (forward CG); (2) thermal control system (high beta); (3) payload deployment and retrieval system (retrieval, a maximum weight, and proximity operations); (4) SSME throttling to 109%; and (5) SSME nozzle entry aerodynamic heating (up elevon/body flap position at hypersonic velocities).


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    Titel :

    Space shuttle status


    Beteiligte:
    Slayton, D. K. (Autor:in)


    Erscheinungsdatum :

    1980-01-01


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Space Shuttle status

    Slayton, D. K. | NTRS | 1979


    Space Shuttle redesign status

    Brand, Vance D. | NTRS | 1986


    Space Shuttle status report.

    Peil, N. G. | NTRS | 1973


    Space Shuttle Transition Management Status

    Henderson, Edward / Norbraten, Gordon | AIAA | 2008


    Space Shuttle Strategic Planning Status

    Henderson, Edward | AIAA | 2007