Feasibility of using rubber base propellants, developed at Jet Propulsion Laboratory, for propulsion of rockets such as WAC Corporal and V-2, is considered; design for high altitude sounding rocket XSPV (i.e., experimental solid propellant vehicle) is presented; propellant, JPL121, is one of series of compositions based on polysulfide rubber as fuel and various quantities of ammonium perchlorate and potassium perchlorate as oxidizers; ballistic data.


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    Title :

    Applicability of solid propellants to high-performance rocket vehicles


    Additional title:

    Astronautics


    Contributors:

    Published in:

    Astronautics ; 7 , n 10


    Publication date :

    1962


    Size :

    7 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




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