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    Paper code

    IAC-17,D2,5,10,x38116

    Date

    2017-09-28

    Time

    09:45

    Order

    10

    Room

    Hall O

    Title

    a hydrogen-turbo-pump-powered thrust vector control servo system for high thrust liquid-hydrogen-liquid-oxygen rocket engines

    abstract

    View PDF

    Session

    5. Technologies for Future Space Transportation Systems

    symposium

    D2. SPACE TRANSPORTATION SOLUTIONS AND INNOVATIONS SYMPOSIUM

    congress

    IAC-17

    Type of presentation

    oral

    Main author

    Mr. Guanghui Jing, China Academy of Launch Vehicle Technology (CALT), China

    Co-authors

    Mrs. Zhang Xiaosha, China Academy of Launch Vehicle Technology (CALT), China;

    Mr. Zeng Guangshang, China Academy of Launch Vehicle Technology (CALT), China;

    Mr. Shoujun Zhao, China Academy of Launch Vehicle Technology (CALT), China;

    Mr. Chuanwei Yin, China Academy of Launch Vehicle Technology (CALT), China;