Paper summarizes significant results of NASA study of 6-12. million-lb thrust launch vehicles (Saturn through Nova Class), at Marshall Space Flight Center, Huntsville, Ala; included are selected study results, summary of vehicle types considered, structural performance, operations, reliability, and economic characteristics; liquid and solid propellant, and nuclear vehicles with orbital and escape mission capabilities.


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    Titel :

    Selection of high thrust launch vehicles


    Weitere Titelangaben:

    SAE -- Paper


    Beteiligte:
    Kolyer, R.C. (Autor:in)

    Kongress:

    SAE Meeting ; 1962 Boosters



    Erscheinungsdatum :

    1962


    Format / Umfang :

    10 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Selection of High Thrust Launch Vehicles

    Kolyer, R. C. | NTRS | 1962


    Selection of High Thrust Launch Vehicles

    Kolyer, R. C. | SAE Technical Papers | 1962



    Take-Off Thrust Augmentation For Reusable Launch Vehicles

    Tanck, P. A. / American Institute of Aeronautics and Astronautics / Society of Automotive Engineers et al. | British Library Conference Proceedings | 1996


    Thrust Vector Control Requirements for Solid- Propellant Launch Vehicles

    J. Borsody / K. I. Davidson / F. Teren | NTIS | 1967