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    Title :

    Effect of Pressure and Propellant Composition on Graphite Rocket Nozzle Erosion Rate


    Contributors:

    Published in:

    Publication date :

    2007



    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    Unknown



    Classification :

    BKL:    55.50 Luftfahrzeugtechnik / 55.50
    Local classification TIB:    770/7040





    feet of Chamber Pressure & Propellant Composition on Erosion Rate of Graphite Rocket Nozzle (AIAA 2006-0363)

    Acharya, R. / Kuo, K. K. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2006