Background and features of system in which tanks are pressurized by means of solid propellant charge, and combined with combustion chamber to form single package in which propellants are self-igniting; principal characteristics such as resistance to environmental conditions; design problems and possible developments with regard to selection of propellants, materials, burning time, ignition and combustion, and safety; possible applications related to missiles, aircraft, and space projects.


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    Title :

    Packaged liquid rocket motors


    Additional title:

    Roy Aeronautical Soc -- J


    Contributors:
    Neat, W.N. (author) / Page, K.G. (author)

    Published in:

    Publication date :

    1962


    Size :

    6 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English






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