Description of some system integration studies which were carried out to define design requirements ensuring compatibility and satisfactory performance of individual Space Shuttle elements. Studies considered include definition of a vehicle concept providing a tradeoff between development and flight costs, evaluation of the need for booster thrust vector control, and analysis of optimum methods for vehicle control in aerodynamic flight.


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    Titel :

    System integration considerations for the Space Shuttle.


    Beteiligte:

    Kongress:

    Short Course on the Space Shuttle Program ; 1972 ; Boulder, CO


    Erscheinungsdatum :

    1973-01-01


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    The Space Shuttle - Key considerations

    Malkin, M. S. | NTRS | 1974


    Space shuttle structural fatigue considerations

    Getline, G. L. / Schaefer, W. H. | NTRS | 1970


    Space Shuttle Cargo Integration Assessments

    Maltby, H. / European Space Agency / United States | British Library Conference Proceedings | 2002


    Space shuttle data handling and communications considerations.

    Stoker, C. J. / Minor, R. G. | NTRS | 1971