Significant design changes made to major components of the NASA Space Shuttle SRM are summarized. The extent of changes made in the nozzle-to-case joint to better protect the joint O-ring seals is indicated schematically as are changes made to the motor nozzle. It is noted that the use of subscale, full scale/short duration burn hardware tests to provide data for structural and thermal analytical models was necessary.


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    Titel :

    Space Shuttle solid rocket motor testing for return to flight


    Beteiligte:
    Coates, Keith D. (Autor:in) / Davis, Carl M. (Autor:in)

    Kongress:

    Aerospace Testing Seminar ; 1988 ; Manhattan Beach, CA, United States


    Erscheinungsdatum :

    1988-01-01


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch




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