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.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    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 :