Problems in meeting basic requirements of efficient conversion of chemical energy locked up in propellants into kinetic energy to supply useful thrust with least possible weight and greatest possible reliability; their effects on range or altitude which can be achieved. (See also Brit Interplanetary Soc -- J v 15 n 3 May-June 1956 p 146-63)


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    Title :

    Combustion chambers for rocket engines


    Additional title:

    Flight


    Contributors:

    Published in:

    Flight ; 69 , n 2460


    Publication date :

    1956


    Size :

    2 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English





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