Uncooled nuclear rocket nozzle would provide significant weight, cost, and reliability advantages; current data on materials indicate that composite materials systems would be capable of successful operation in extreme environments imposed on nuclear rocket nozzles; four-basic-composite-materials-systems concept which has been developed under preliminary program sponsored by Martin-Orlando.


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    Titel :

    Material design concepts for uncooled nuclear rocket nozzles


    Weitere Titelangaben:

    Matls Science Research


    Beteiligte:
    Locke, S.R. (Autor:in) / Ahearn, R.L. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1965


    Format / Umfang :

    24 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Uncooled Rocket Nozzles for Ultra-High Temperature Propellants

    Kraus, George | SAE Technical Papers | 1962



    Multiple exhaust nozzles for nuclear rocket engines

    DUKE, E. / VANICA, D. | AIAA | 1966


    Advanced Rocket Nozzles

    Hagemann, G. / Immich, H. / Nguyen, T. V. et al. | British Library Conference Proceedings | 1998


    Advanced Rocket Nozzles

    Gerald Hagemann / Hans Immich / Thong Van Nguyen et al. | AIAA | 1998