Paper presents approach for expanding capability and flexibility of Saturn V vehicle, which is destined for lunar landing mission, by adding varying numbers and sizes of solid-propellant strap-on rocket motors (SRMs); design studies using 120-, 156-, and 260-in. diam strap-on motors led to concept; family of vehicles defined has range of payload capabilities extending from current uprated Saturn I to well beyond that of Saturn V; unit payload-to-orbit costs for concept are compared with those of other proposed methods for augmentation of Saturn V; comparisons demonstrate that concept offers high payload capability and mission flexibility within reasonable development schedule for minimal overall program cost.


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    Titel :

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


    Weitere Titelangaben:

    J Spacecraft Rockets


    Beteiligte:
    Monroe, J.W. (Autor:in) / Corso, C.J. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1968


    Format / Umfang :

    6 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :




    Selected methods for uprating Saturn vehicles.

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


    Selected methods for uprating Saturn vehicles

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


    Selected Methods for Uprating Saturn Vehicles

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