Capabilities of number of launching systems are reviewed, and some current United States spacecraft listed to indicate range of missions that are feasible; considerations which influence choice of new launching system to meet possible requirement for European vehicle are discussed, with particular reference to effects of booster stage recovery on economics; five expendable launching systems, and one using recoverable booster stage are considered; estimates are made of relative costs per pound in orbit; some possible trends in propulsion system development.


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    Title :

    Aerospace applications of rocket engines


    Additional title:

    Brit Interplanetary Soc -- J


    Contributors:
    Maher, L.E. (author)


    Publication date :

    1964


    Size :

    9 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :



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