High purity silica reinforced ablative composite materials evaluated as nozzle sections of throat storable propellant rocket engine - erosion rates and charring


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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 :

    1967-06-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English