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  • GLEX-2017
  • 7
  • 2
  • session 2

    Title

    Entering into Space and New Energy and Propulsion Technology

    type

    oral

    Date

    2017-06-07

    Time

    17:00

    Room

    203 D

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    4

    Computational technology application for solid rocket motor burn simulation

    13

    withdrawn

    Mr. Guilherme Mejia

    Instituto Tecnológico de Aeronáutica (ITA)

    Brazil

    5

    design of a throttleable hybrid rocket propulsion platform for planetary soft landing

    13

    confirmed

    Dr. Sheng Zhao

    China Academy of Launch Vehicle Technology (CALT)

    China

    6

    Orion European Service Module Propulsion Subsystem on Fire

    13

    withdrawn

    Mr. Markus Jäger

    Airbus Defence & Space, Space Systems

    Germany

    7

    Simple Guidance Scheme for Low-Thrust Geostationary Orbit Transfers

    13

    Dr. Xue Ma

    Beijing Institute of Control Engineering, China Academy of Space Technology (CAST)

    China

    9

    Reusable Launch Vehicle-Concept of Minimizing Space Transportation Cost

    13

    withdrawn

    Mr. Nadeem Alam

    Department of Aeronautical Engineering, Babu Banarsi Das National Institute of Technology and Management, Lucknow,

    India

    12

    Thermodynamic Performance of 250kW Space Nuclear Power System Based on Liquid Metal Rankine Cycle

    13

    confirmed

    Prof.Dr. Haochun Zhang

    Harbin Institute of Technology

    China

    13

    Laser Ablation Propulsion Launch System (LAPLaS) Potentialities.

    13

    withdrawn

    Mr. IOURI PIGULEVSKI

    Switzerland

    16

    parametric analysis of a 30kN thrust class for nuclear thermal engine(nte)system

    13

    confirmed

    Ms. Haoze Wang

    Beijing Aerospace Propulsion Institute

    China

    17

    The studying of neutralizer characterization of multi-throttling point ion engine

    13

    withdrawn

    Dr. yanhui jia

    Lanzhou Institute of Physics

    China

    20

    Research on Anode Power Supply Technology with High - gain and Wide - range Output Voltage for Hall Electric Propulsion System

    13

    confirmed

    Mrs. Huiying Liu

    State Key Laboratory of space power supply technology

    China