Ablative material degradation in liquid propellant rocket engine environment of nitrogen tetroxide-aerozine


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    Title :

    Experimental and theoretical analysis of ablative material response in a liquid- propellant rocket engine Final report


    Contributors:
    Clark, K. J. (author) / Flood, D. T. (author) / Moyer, C. B. (author) / Rindal, R. A. (author)

    Publication date :

    1967-09-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English