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    Paper code

    IAC-17,D2,4,8,x38809

    Place

    2017-09-27 14:45, #8, Hall O

    Title

    A Conceptual Analysis and Comparison of a Two-Stage-To-Orbit Reusable Launch Vehicle Using Airbreathing Precooling Hypersonic Engines

    abstract

    View PDF

    Session

    4. Future Space Transportation Systems

    symposium

    D2. SPACE TRANSPORTATION SOLUTIONS AND INNOVATIONS SYMPOSIUM

    congress

    IAC-17

    Type of presentation

    oral

    Main author

    Dr. Jianxing Zhou, Beijing Aerospace Technology Institute, China

    Co-authors

    Ms. Hong LU, Beijing Aerospace Technology Institute, China;

    Mr. Haocheng ZHANG, Beijing Aerospace Technology Institute, China;

    Mr. Lingbo ZHAO, Beijing Aerospace Technology Institute, China;

    Ms. Jingmin CHEN, Science and Technology on Scramjet Laboratory, Beijing Power Machinery Research Institute, China;

    Dr. Riheng Zheng, Science and Technology on Scramjet Laboratory, Beijing Power Machinery Research Institute, China;