Protection against malfunctions in flight control system is provided by redundant flight control system with automatic and manual switchover provisions from primary to secondary system; malfunctions of other vital systems of launch vehicle require abort, and manually initiated crew escape means are provided; operation of flight control switchover mechanism for several classes of malfunctions, and criteria developed for judging conditions under which switchover can be accomplished; on-board and ground warning displays for nonflight control malfunctions and time sequence of escape events for critical malfunction.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Malfunction protection in gemini launch vehicle


    Weitere Titelangaben:

    Symposium Ballistic Missile Space Technology -- Trans


    Beteiligte:
    Hecht, H. (Autor:in)

    Kongress:

    8th Symposium on Ballistic Missile and Space Technology ; 1963 Reliability



    Erscheinungsdatum :

    1963


    Format / Umfang :

    45 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :