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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    Title :

    Rocket nozzle development


    Additional title:

    Aeroplane Astronautics


    Contributors:
    Bunting, D. (author)

    Published in:

    Publication date :

    1962


    Size :

    3 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :




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