Reevaluation of Vanguard program objectives in Jan 1957 resulted in production of 6.44-in. diam, 3.25-lb sphere with 6 equally spaced solar cell clusters and 6 antennas mounted on its surface; development of mechanism to separate satellite from third-stage rocket; satellite and strap pull pin girth ring arrangement were fully tested prior to flight; successful orbiting and flight operation proved adequacy of design.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Vanguard I satellite structure and separation mechanism


    Weitere Titelangaben:

    NASA -- Tech Note


    Beteiligte:
    Shea, J.T. (Autor:in) / Baumann, R.C. (Autor:in)


    Erscheinungsdatum :

    1961


    Format / Umfang :

    13 pages


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Vanguard I Satellite Structure and Separation Mechanism

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


    Vanguard I satellite structure and separation mechanism

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


    Vanguard I Satellite Structure and Separation Mechanism

    J. T. Shea / R. C. Baumann | NTIS | 1961


    Vanguard satellite separation mechanisms

    Baumann, R.C. | Engineering Index Backfile | 1961


    Vanguard Satellite Separation Mechanisms

    R. C. Baumann | NTIS | 1961