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  • session 5

    Title

    Hypersonic and Combined Cycle Propulsion

    type

    oral

    Description

    This session includes papers dealing with use of air in earth-to-orbit propulsion.

    Date

    2012-10-04

    Time

    10:15

    Room

    TS14 (Sala Capri, Palacongressi)

    IPC members
    • Chairman: Prof. Shigeru Aso, Kurume Institute of Technology, Japan;

    • Chairman: Dr. Salvatore Borrelli, CIRA Italian Aerospace Research Centre, Italy;

    • Rapporteur: Mr. Patrick Danous, ArianeGroup, France;

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    Aero-spike and RBCC Engine Systems for Future Space Transportation Vehicle

    15'

    confirmed

    Mr. Tetsuo Hiraiwa

    Japan Aerospace Exploration Agency (JAXA)

    Japan

    4

    Ramjet thruster using ozone dissociation energy for high altitude operation

    15'

    confirmed

    Mr. Florin Mingireanu

    Romanian Space Agency (ROSA)

    Romania

    7

    An experimental study on highly efficient ddt enhancement device for pde

    15'

    confirmed

    Mr. Ryuji NAKAWATASE

    Kyushu University

    Japan

    10

    Numerical and experiment study of the dynamic work process of a new type two-stage supersonic air ejector

    15'

    confirmed

    Ms. Jie Huang

    China Aerodynamics Research and Development Center (CARDC) 

    China

    10

    Numerical and experiment study of the dynamic work process of a new type two-stage supersonic air ejector

    15'

    confirmed

    Mr. Zonghao Wang

    China Aerodynamics Research and Development Center (CARDC) 

    China

    12

    Analysis of the first stage trajectory for a TSTO space transportation concept powered by RBCC engine

    Poster

    confirmed

    Mr. RUI XUE

    College of Astronautics, Northwestern Polytechnical University

    China

    13

    Aerodynamic Characteristics Research on the Waverider-based Hypersonic Vehicle with the Grid Fin

    Poster

    confirmed

    Mr. Qing-Yang Guo

    National University of Defense Technology

    China

    14

    Thrust measure and capability analysis of H2/air mixture continuous rotating detonation wave model engine

    Poster

    Mr. Wei Lin

    College of Aerospace and Materials Engineering, National University of Defense Technology

    China

    16

    Quasi-two-dimensional evaluation and optimization design for hypersonic scramjet propulsive flowpath

    Poster

    confirmed

    Mr. Xin Ren

    Science and Technology on Scramjet Laboratory, The 31st Research Institute of CASIC

    China