Examination of effect of varying exhaust gas velocity so that exhaust gases possess little or no kinetic energy in earth observer's frame of reference; under certain boundary conditions improvement in terminal velocity of 10 to 20% is obtained relative to rocket with fixed exhaust velocity.


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    Title :

    Performance of rocket with tapered exhaust velocity


    Additional title:

    Jet Propulsion


    Contributors:

    Published in:

    Jet Propulsion ; 27 , n 12 ; p 1264-1266


    Publication date :

    1957


    Size :

    3 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




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