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    Title :

    The Effects of Oxidizer Injector Design on Hybrid Rockets Combustion Stability


    Contributors:

    Conference:

    42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit



    Publication date :

    2006-01-01




    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English




    The Effects of Oxidizer Injector Design on Hybrid Rockets Combustion Stability

    Carmicino, C. / Sorge, A. R. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2006




    Optimal Design of Hybrid Rockets with Self-Pressurizing Oxidizer

    Casalino, Lorenzo / Pastrone, Dario | AIAA | 2006


    Optimal Design of Hybrid Rockets with Self-Pressurizing Oxidizer

    Casalino, L. / Pastrone, D. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2006