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    Title :

    Assessing Oxidizer Injector Design via Thermochemical Imaging of PMMA Combustion in a Hybrid Rocket Motor Geometry



    Conference:

    AIAA Propulsion and Energy 2020 Forum



    Publication date :

    2020-01-01



    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English



    ASSESSING OXIDIZER INJECTOR DESIGN VIA THERMOCHEMICAL IMAGING OF PMMA COMBUSTION IN A HYBRID ROCKET MOTOR GEOMETRY

    Sanders, Isabelle C. / Bendana, Fabio A. / Hagstrom, China et al. | TIBKAT | 2020


    Variable-flow hybrid rocket oxidizer injector

    Robertson, David / Mueller, Paul | AIAA | 2001


    Oxidizer injector for motor

    CHEN YEN-SEN | European Patent Office | 2022

    Free access

    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


    The Effects of Oxidizer Injector Design on Hybrid Rockets Combustion Stability

    Carmicino, Carmine / Russo Sorge, Annamaria | AIAA | 2006