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  • IAC-15
  • D2
  • IP
  • session IP

    Title

    Interactive Presentations

    type

    interactive

    Date

    2015-10-14

    Time

    13:15

    IPC members
    • Coordinator: Dr. John M. Horack, The Ohio State University College of Engineering, United States;

    • Coordinator: Mr. Ulf Palmnäs, Swedish Space Corporation (SSC), Sweden;

    papers

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    Standardization of Small Satellite Launch Services

    confirmed

    Mr. Abhijeet Gahlot

    India

    Designing and Testing Parachute Recovery System for Sounding Rocket

    confirmed

    Mr. Blazej Marciniak

    Institute of Aviation

    Poland

    On a method of controlling the angle of entry in the atmosphere

    withdrawn

    Mr. Maxim Dzhabarov

    Russian Federation

    The Method for Calculate Added Mass of Parachute

    withdrawn

    Mr. Huang Wei

    Beijing Institute of Mechanical & Electrical Engineering

    China

    THE APPLICATION OF UPPER STAGES IN SPACE MISSIONS

    Mr. Feng QI

    Beijing Institute of Aerospace Systems Engineering, China Aerospace Science and Technology Corporation (CASC)

    China

    Innovative launch vehicle technologies

    confirmed

    Mr. Borys Kovalov

    Ukraine

    RING ROCKETS

    confirmed

    Mr. Oleg Aleksandrov

    AVIASTAR Inc www.aviastar.us

    United States

    the choice of candidate launchers for operation from a national spaceport

    confirmed

    Mr. Gerald Webb

    Commercial Space Technologies Ltd.

    United Kingdom

    Integrated automated system as one of the key elements of the Vostochny cosmodrome operation system

    confirmed

    Mrs. Alla Serikova

    Central Research Institute of Machine Building (FSUE/TSNIIMASH)

    Russian Federation

    A Practical Model of CMOS Integrated Hall sensor

    Mrs. Bai xiaohe

    China

    Framework Design of Aerospace Vehicles Common Mission Planning System for Plan Optimization

    confirmed

    Mr. Ziyang Song

    Beijing Electro-Mechanical Engineering Institute, China Aerospace Science & Industry Corporation (CASIC)

    China

    study on the flow coefficient relation between helium and nitrogen of orifice plate used in rocket pressurization system

    withdrawn

    Mr. Wang Huilong

    Beijing Aerospace Institute of Metrology & Measurement Technology

    China

    responsive test technology for chinese next generation launch vehicle

    confirmed

    Prof. Zhengyu Song

    China Academy of Launch Vehicle Technology (CALT)

    China

    fast terminal sliding mode attitude control for hypersonic flight vehicle with disturbance observer

    confirmed

    Dr. Jie Liang

    China

    RENEWABLE ENERGY BASED SPACE COLONY

    confirmed

    Mr. SOURAV KARMAKAR

    India