Features of strap, pull pin, girth ring separation device; residual burning of third-stage made it necessary to delay separation longer than time designed into long-delay separation device; standard separation mechanism was modified and integrated with satellite command receiver system so that ground command after third stage burnout would cause separation.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Vanguard satellite separation mechanisms


    Additional title:

    NASA -- Tech Report


    Contributors:


    Publication date :

    1961


    Size :

    20 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English




    Vanguard Satellite Separation Mechanisms

    Baumann, Robert C. | NTRS | 1961


    Vanguard satellite separation mechanisms

    Baumann, Robert C. | TIBKAT | 1961


    Vanguard Satellite Separation Mechanisms

    R. C. Baumann | NTIS | 1961


    Vanguard satellite

    Furnas, C.C. | Engineering Index Backfile | 1957


    Vanguard I Satellite Structure and Separation Mechanism

    Shea, John T. / Baumann, Robert C. | NTRS | 1961