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  • session 3

    Title

    Hypervelocity Impacts and Protection

    Description

    The session will address passive protection, shielding and damage predictions. Shielding aspects will be supported by experimental and computational results of HVI tests.

    Date

    2010-09-29

    Time

    10:15

    Room

    Terrasse 2

    IPC members
    • Chairman: Dr. V. Adimurthy, Indian Space Researh Organisation, India;

    • Chairman: Dr. Hedley Stokes, PHS Space Ltd, United Kingdom;

    • Rapporteur: Dr. Carsten Wiedemann, TU Braunschweig, Institute of Space Systems, Germany;

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    Shuttle Post Flight MMOD Inspection Highlights

    18

    confirmed

    Mr. James Hyde

    Barrios Technology/ESC Group - NASA

    United States

    2

    A Study of Plasma Accelerator using Pulse Power for Hypervelocity Impact Test

    18

    withdrawn

    Dr. Tomohiro Narumi

    Kyushu Institute of Technology

    Japan

    3

    The Study of Hypervelocity Impact Character for Honeycomb Sandwich with Multi-Layer Insulation

    18

    confirmed

    Ms. Jie Huang

    China Aerodynamics Research and Development Center (CARDC) 

    China

    4

    Oblique Hypervelocity Impact Experiment for Spacecraft Debris Shield

    18

    confirmed

    Dr. Koji Tanaka

    Japan Aerospace Exploration Agency (JAXA)

    Japan

    5

    Fragmentation of hypervelocity aluminum projectiles on fabrics

    18

    confirmed

    Mr. Martin Rudolph

    Fraunhofer EMI

    Germany

    6

    Experimental Comparison of Al Sphere Hypervelocity Impact on Al-foam Sandwiched Shield and Al-foam Stuffed Shield

    18

    confirmed

    Dr. Bin Jia

    Harbin Institute of Technology

    China

    7

    the hypervelocity impact test investigation and analysis on thermal control instrument in the satellites

    18

    confirmed

    Ms. Yuhua Huo

    China Academy of Space Technology (CAST)

    China

    8

    STUDY OF HYPERVELOCITY IMPACT ON ELECTRODYNAMIC TETHER FOR TETHER LIFETIME EVALUATION

    18

    confirmed

    Mr. Atsushi Yanagida

    Waseda University

    Japan

    9

    A Ballistic Limit Analysis Program for Shielding Against Micrometeoroids and Orbital Debris

    18

    confirmed

    Mr. Shannon Ryan

    Defence Science and Technology Organisation (DSTO)

    Australia

    10

    damage identification of single aluminum plate produced by hypervelocity impact based acoustic emission

    18

    confirmed

    Dr. Wugang Liu

    Beijing Institute of Structure and Environmental Engineering (BISE)

    China