Uprated Saturn I is composed of two propulsion stages, designated S-IB and S-IVB stages, and Instrument Unit; methods of providing increased payload together with vehicle uprating studied by Chrysler Corp Space Div and NASA include propellant substitution, S-IB stage propellant tank extensions, and addition of strap-on solid propellant rocket motors for thrust augmentation; additional upper stages as potential uprating techniques and combinations of solid rocket motors and additional upper stages are reviewed; analysis shows that uprating is feasible up to 106,000 1b payload into low earth orbit and up to 25,000 lb on Mars mission.


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    Titel :

    Further uprating of Saturn I for missions of future


    Weitere Titelangaben:

    SAE -- Paper


    Beteiligte:
    Buell, D.N. (Autor:in) / Schnyder, A.S. (Autor:in)

    Kongress:

    SAE Meeting ; 1966



    Erscheinungsdatum :

    1966


    Format / Umfang :

    6 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Further Uprating of Saturn I For Missions of the Future

    Schnyder, Albert S. / Buell, David N. | SAE Technical Papers | 1966


    Selected methods for uprating Saturn vehicles

    Orillion, A.G. / Scott, R.D. | Engineering Index Backfile | 1966


    Selected methods for uprating Saturn vehicles.

    Orillion, A. G. / Scott, R. D. | NTRS | 1966


    Selected Methods for Uprating Saturn Vehicles

    Orillion, Alfred G. / Scott, Ronald D. | SAE Technical Papers | 1966


    Building-block approach to saturn V uprating using solid-propellant motors

    Monroe, J.W. / Corso, C.J. | Engineering Index Backfile | 1968