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  • IAC-08
  • C2
  • 6
  • session 6

    Title

    Space Environmental Effects and Spacecraft Protection

    type

    oral

    Description

    In this session space environment effects will be covered. For example, the effects of radiation, atomic oxygen, spacecraft charging, thermal cycling, dissociation, meteoroids, space debris and vacuum on space systems, microelectronics, materials and structures will be discussed. Protective and shielding technologies, including debris impact simulation, testing and susceptibility of Commercial-Off-The-Shelf (COTS) micro-electronics to space radiation will be presented.

    Date

    2008-10-02

    Time

    10:00

    Room

    Dochart 1

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

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

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    NUMERICAL SIMULATION OF IMPACT LOADING ON ELASTIC SPACE STRUCTURE AND CASE STUDIES

    presentation

    Prof. Harijono Djojodihardjo

    Universitas Al Azhar Indonesia

    Indonesia

    3

    Influence Factors of Temperature Difference between Ground Thermal Balance Test and Orbit Data of Spacecraft

    presentation

    Mr. jun jiang

    China Academy of Space Technology (CAST)

    China

    4

    Impact detection onboard satellites using wireless sensor network

    presentation

    Dr. Frank Schäfer

    Fraunhofer EMI

    Germany

    5

    Development of Electron Emitting Film for Spacecraft Charging Mitigation II Improvement of Performance

    presentation

    Dr. Minoru Iwata

    Kyushu Institute of Technology

    Japan

    6

    Investigation into Tolerance of Polysiloxane-Block-Polyimide Film against Atomic Oxygen

    presentation

    Dr. Eiji Miyazaki

    Japan Aerospace Exploration Agency (JAXA)

    Japan

    7

    Low CTE Waveguide for Extreme Thermal Environment

    presentation

    Mr. Sandro Mileti

    University of Rome “La Sapienza”

    Italy

    8

    A Small Low-Cost Resistance Based Atomic Oxygen Sensor

    presentation

    Prof. Jingyu Tong

    Beijing institute of satellite environment engineering

    China

    9

    Development Status and Prospect of TPS for RLV

    Mr. Ting Liu

    The 7th Academy, China Aerospace Science and Technology Corporation (CASC)

    China

    10

    Analysis of the Long-Term Evolution of Satellite Temperatures by Analysing of its Thermal Behavior in Orbit

    discussion

    Ms. Andreia Sorice

    INPE

    Brazil

    11

    development of spacecraft charging measuring instrument with parallel plate electrostatic energy analyzer

    presentation

    Dr. Naomi Kurahara

    University of Tokyo

    Japan