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 Flight v 69 n 2460 Mar 16 1956 p 299-300)


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    Title :

    Combustion chambers for rocket engines


    Additional title:

    Brit Interplanetary Soc -- J


    Contributors:


    Publication date :

    1956


    Size :

    18 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




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