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    Title :

    Design of a N20/HTPB Hybrid Rocket Motor Utilizing a Toroidal Aerospike Nozzle


    Contributors:

    Conference:

    48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition



    Publication date :

    2010-01-01




    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English




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