Access

    Access via TIB

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    EXPERIMENTAL INVESTIGATION OF A FLOW-ORIENTED THROTTLEABLE INJECTOR DESIGNED FOR THROTTLEABLE HYBRID ROCKET MOTOR


    Contributors:
    Zhao, Zeng (author) / Cai, Guobiao (author) / Zhao, Bo (author) / Liu, Yufei (author) / Yu, Nanjia (author)

    Conference:

    IAF Space Propulsion Symposium ; 2020 ; Online



    Publication date :

    2021



    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English



    Classification :

    BKL:    55.60 Raumfahrttechnik




    AXISYMMETRIC, THROTTLEABLE NON-GIMBALLED ROCKET ENGINE

    Sackheim, Robert L. / Hutt, John J. / Anderson, William E. et al. | NTRS | 2005


    Experimental Tests of Throttleable H2O2/PE Hybrid Rocket Motors

    Zhao, Sheng / Cai, Guobiao / Tian, Hui et al. | AIAA | 2015


    Experimental Investigation of Throttleable H 2 O 2 and Polypropylene Hybrid Rocket Motor

    Li, Meng-Che / Chang, Chih-Shin / Wei, Shih-Sin et al. | AIAA | 2023


    Modelling of a Throttleable Ducted Rocket Propulsion System

    Bauer, Chistoph / Davenne, Francois / Hopfe, Norman et al. | AIAA | 2011