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    Title :

    Hybrid rocket combustion regression rate model.


    Author / Creator :

    MILLER, E. /LOCKHEED AIRCRAFT CORP., LOCKHEED MISSILES AND SPACE CO., RESEARCH LAB., PALO ALTO, CALI


    Contributors:
    MILLER, E. (author)

    Published in:

    AIAA Journal ; 4 , 4 ; 752-753


    Publication date :

    1966-01-01


    Size :

    2 pages




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English




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