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  • session 6

    Title

    Space Environmental Effects and Spacecraft Protection

    Description

    The focus of the session will be on space environmental effects and spacecraft protection. The effects of vacuum, radiation, atomic oxygen, spacecraft charging, thermal cycling, dissociation, meteoroids and space debris impact on space systems, materials and structures, and microelectronics will be addressed. Protective and shielding technologies, including analysis simulation and testing of debris impact, and susceptibility of Commercial-Off-The-Shelf (COTS) micro-electronics to space radiation will be covered.

    Date

    2009-10-15

    Time

    10:00

    Room

    Technical Session #5

    IPC members
    • Chairman: Dr. Minoo Dastoor, National Aeronautics and Space Administration (NASA), United States;

    • Chairman: Prof. Akira Meguro, Tokyo City University, Japan;

    • Rapporteur: Dr. Giuliano Marino, CIRA Italian Aerospace Research Centre, Italy;

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    ANALYSIS AND SIMULATION OF IMPACT LOADING ON LARGE ELASTIC SPACE STRUCTURE

    20'

    Prof. Harijono Djojodihardjo

    Universitas Al Azhar Indonesia

    Indonesia

    2

    Influence of Ply Angle on the Fabrication Stresses of Composite Tubes Used in Space Applications

    20'

    Mr. Geoffrey Milburn

    Royal Military College

    Canada

    4

    The SARG Methodology: Upgrading Solar Energetic Particle Event Time Distributions and Modelling Methods

    20'

    Mr. Piers Jiggens

    University of Southampton

    United Kingdom

    5

    Development of spacecraft surface contamination sensors

    20'

    Prof. Kazutaka Nishiyama

    Japan Aerospace Exploration Agency (JAXA)

    Japan

    6

    development of the protecting high voltage solar array base plate from atomic oxygen

    20'

    Prof. Jingyu Tong

    Beijing institute of satellite environment engineering

    China

    7

    Electron-emitting Film, an effective mitigation of spacecraft charging through the field emission

    20'

    Dr. Arifur Khan

    Japan

    8

    The Sectional Optimization Design of High Speed Aircraft at Ablation Thermal Protection

    20'

    Dr. Yin LianHua

    China

    9

    Atomic Oxygen facility simulating LEO AO environment for material exposure to understand charging-arching behavior of exposed surface materials

    20'

    Mr. NOOR DANISH AHRAR MUNDARI

    Kyushu Institute of Technology

    Japan

    10

    Preliminary study of development of space debris removal method using electrostatic force

    20'

    Mr. Yasunori Furukawa

    Kyushu Institute of Technology

    Japan

    11

    Space Environmental Issues in Developing Wireless Smallsat Data Bus

    20'

    Dr. Yunlong Lin

    York University

    United States