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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. Use of HVI techniques for debris mitigation.

    Date

    2011-10-05

    Time

    15:00

    Room

    TS-15

    IPC members
    • Chairman: Dr. Sergey Meshcheryakov, TSNIIMASH, Russian Federation;

    • Chairman: Dr. Frank Schäfer, Fraunhofer EMI, Germany;

    • Rapporteur: Mr. James Hyde, Barrios Technology/ESC Group - NASA, United States;

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    Hypervelocity Impact Testing of Advanced Materials and Structures for Micrometeoroid and Orbital Debris Shielding

    15

    confirmed

    Dr. Shannon Ryan

    Defence Science and Technology Organisation (DSTO)

    Australia

    2

    Verification on hypervelocity impact tests of ejecta and data analysis of witness plates after the impact tests

    15

    confirmed

    Prof.Dr. Yasuhiro Akahoshi

    Kyushu Institute of Technology

    Japan

    3

    Interpretation of impact features on the surface of the WFPC-2 radiator

    15

    withdrawn

    Dr. Phillip Anz-Meador

    ESCG/Jacobs

    United States

    4

    Electrical response of current-carrying space-grade harnesses to hypervelocity impact

    15

    confirmed

    Mr. Martin Rudolph

    Fraunhofer EMI

    Germany

    5

    Electrical breakdowns on SC surfaces due to microparticles impacts

    15

    withdrawn

    Dr. Sergey Meshcheryakov

    TSNIIMASH

    Russian Federation

    6

    Electrical Effects of Hypervelocity Impacts

    15

    confirmed

    Mr. Ashish Goel

    Stanford University

    United States

    7

    Shuttle Hypervelocity Impact Database

    15

    confirmed

    Mr. James Hyde

    Barrios Technology/ESC Group - NASA

    United States

    8

    Fragment Characteristic of Simulated Spacecraft under Hypervelocity Impact

    15

    confirmed

    Mr. SHENGWEI LAN

    China Aerodynamics Research and Development Center (CARDC) 

    China

    9

    Improvements for Space Mission Protection against Space-Debris Hazards

    15

    confirmed

    Mr. Jeffrey Apeldoorn

    OHB System AG

    Germany

    10

    Computational Methodology to Predict Satellite System-level Effects from Untrackable Space Debris

    15

    confirmed

    Mr. Nathan Welty

    Fraunhofer EMI

    Germany

    11

    DEVELOPMENT OF IN-SITU MICRO-DEBRIS MEASUREMENT SYSTEM

    15

    confirmed

    Dr. Yukihito Kitazawa

    IHI Corporation

    Japan

    12

    Development of an implosion-driven hypervelocity launcher for orbital debris and micrometeoroid simulation

    15

    confirmed

    Mr. Justin Huneault

    McGill University

    Canada

    21

    SHIELDED AND UNSHIELDED LOOP HEAT PIPE IN SPACECRAFT TO HYPERVELOCITY IMPACTS

    15'

    confirmed

    Ms. Yuhua Huo

    China Academy of Space Technology (CAST)

    China