Critical phases of flight that define characteristics of recovery system are conditions and requirements between stage separation to re-entry, re-entry, and terminal descent and landing; vehicle considerations that must be investigated in establishing requirements of recovery system are presented; review of programs initiated at NASA Marshall Space Flight Center, to substantiate recovery program for launch vehicles, viz, H-1 engine salt water immersion tests and booster retrieval exercises at sea.


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    Titel :

    Launch vehicle recovery system requirements


    Weitere Titelangaben:

    SAE -- Paper


    Beteiligte:
    Barraza, R.M. (Autor:in)

    Kongress:

    SAE Meeting ; 1962 Recovery



    Erscheinungsdatum :

    1962


    Format / Umfang :

    6 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :



    Launch Vehicle Recovery System Requirements

    Barraza, R. M. | SAE Technical Papers | 1962



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    Ragab, Mohamed / Cheatwood, F. McNeil | AIAA | 2015


    Launch vehicle integration requirements for SP-100

    L. T. Shaw / J. R. Womack | NTIS | 1984