Development of uncooled nozzles for missiles and space boosters requiring nozzle of large throat diameter to withstand gas temperature greater than 3200 K for 3 min for first stage and expansion cone of small dimensions to meet gas temperature of 1500 K under conditions of high heat transfer since liquid hydrogen will be fuel for third stage; mechanisms responsible for nozzle failure; testing of nozzle materials. Abstract of paper before meeting Nov 22 1961 of Brit Interplanetary Soc.


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    Titel :

    Rocket nozzle development


    Weitere Titelangaben:

    Aeroplane Astronautics


    Beteiligte:
    Bunting, D. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1962


    Format / Umfang :

    3 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :




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