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    Title :

    Experimental Evaluation of High-Purity-Silica Reinforced Ablative Composites as Nozzle Sections of 7.8-Inch-/19.8 cm/ Diameter Throat Storable-Propellant Rocket Engine


    Contributors:

    Publication date :

    1967


    Size :

    28 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English