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    Title :

    Design and Analysis of a Reusable N2O-Cooled Aerospike Nozzle for Labscale Hybrid Rocket Motor Testing


    Contributors:

    Conference:

    47th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit



    Publication date :

    2011-01-01




    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English





    Development of a Reusable Aerospike Nozzle for Hybrid Rocket Motors

    Lemieux, P. / American Institute of Aeronautics and Asronautics | British Library Conference Proceedings | 2009


    Results of Labscale Hybrid Rocket Motor investigation

    Greiner, B. / Frederick, R. A., Jr. | NTRS | 1992


    Labscale hybrid uncertainty analysis (hybrid rocket engines)

    Greiner, B / Frederick, r, R | AIAA | 1995


    Results of Labscale Hybrid Rocket Motor investigation

    GREINER, B. / FREDERICK, JR., R. | AIAA | 1992