Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    High-diodicity impinging injector design for rocket propulsion enabled by additive manufacturing


    Contributors:

    Conference:

    AIAA SCITECH 2022 Forum



    Publication date :

    2022-01-01



    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English



    RDC Operation with Varying Air Injector Diodicity

    Barnouin, Provence / Bach, Eric / Paschereit, Christian Oliver et al. | AIAA | 2024


    The impinging-type injector design of MMH/NTO liquid rocket engine

    Yuan, Tony / Chen, Cetera / Huang, Berlin et al. | AIAA | 2012




    A Cold-flow Experimental Observation of the Two-stage Impinging Type Injector for Rocket Propulsion (AIAA 2015-3765)

    Huang, Berlin / Yuan, Tony / Chen, Yu-Ta et al. | British Library Conference Proceedings | 2015