Selfigniting hybrid rocket propellant system employing 90% hydrogen peroxide as oxidizer and polyethylene as fuel; reasoning which led to this choice and advantages achieved; results obtained in tests with one type of fuel charge; qualitative discussion on operation.


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    Title :

    Solid-liquid rocket propellant system


    Additional title:

    Jet Propulsion


    Contributors:
    Moore, G.E. (author) / Berman, K. (author)

    Published in:

    Jet Propulsion ; 26 , n 11


    Publication date :

    1956


    Size :

    4 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




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