Process of calculation with regard to probable size and first stage thrust for Sputnik launching vehicle is attempted, assuming vehicle to be "standard" 3-stage tandem rocket; assumptions regarding fuel and oxidizer used; trajectory is approximated by trolley car equations; table shows comparison of Vanguard and Sputnik; payload optimization for Sputnik III. (No. Calif Sec) (see also abstract in SAE -- J v 67 n 4 Apr 1959 p 90-1)


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    Titel :

    Comparison of Vanguard and Sputnik launching vehicles


    Weitere Titelangaben:

    SAE -- Paper


    Beteiligte:
    Kramer, S.B. (Autor:in)

    Kongress:

    SAE Meeting ; 1958 Launching



    Erscheinungsdatum :

    1958


    Format / Umfang :

    10 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Comparison of Vanguard and Sputnik launching vehicles

    Kramer, S.B. | Engineering Index Backfile | 1959


    COMPARISON OF VANGUARD AND SPUTNIK LAUNCHING VEHICLES

    KRAMER, SAUNDERS B. | SAE Technical Papers | 1958


    Sputnik and Vanguard: comparison

    Koelle, H.H. | Engineering Index Backfile | 1957


    Sequence diagram analysis of vanguard satellite launching vehicle

    Escher, W.J.D. / Foster, R.W. | Engineering Index Backfile | 1961