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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

    2015-10-14

    Time

    09:45

    Room

    Eshkol 2 (ICC, lower level)

    IPC members
    • Co-Chair: Mr. Frank Schaefer, Fraunhofer - Institut für Kurzzeitdynamik, Ernst-Mach-Institut (EMI), Germany;

    • Co-Chair: Dr. Norman Fitz-Coy, University of Florida, United States;

    • Rapporteur: Prof. Alessandro Francesconi, University of Padova - DII/CISAS, Italy;

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    09:45

    A new Ballistic Limit Equation for thin tape tethers

    18'

    confirmed

    Prof. Alessandro Francesconi

    University of Padova - DII/CISAS

    Italy

    2

    10:03

    Experimental and Numerical Investigations of Stuffed Whipple Shields Protecting Chinese Manned Spacecraft against Orbital Debris

    18'

    confirmed

    Dr. Li Shan

    Institute of Spacecraft System Engineering,China Academy of Space Technology (CAST)

    China

    3

    10:21

    preliminary study on the performance of shielding configuration with stuffed layer under hypervelocity impact

    18'

    confirmed

    Mr. Fa-wei Ke

    China Aerodynamics Research and Development Center (CARDC) 

    China

    4

    10:39

    Simplified S/C vulnerability assessments at component level in early design phase at ESA’s CDF

    18'

    confirmed

    Mr. Scott Kempf

    Fraunhofer - Institut für Kurzzeitdynamik, Ernst-Mach-Institut (EMI)

    Germany

    5

    10:57

    Electrical Phenomena caused by Hypervelocity Impact

    18'

    confirmed

    Dr. Tanaka Koji

    ISAS/JAXA

    Japan

    6

    11:15

    Integration of a Dust Accelerator into the IPG6-B Facility for Material Impact Tests

    18'

    confirmed

    Mr. Christoph Montag

    Institute of Space Systems, Universität Stuttgart

    Germany

    8

    11:33

    experimental study for Laser-driven flyer plates up to 8 km/s

    18'

    confirmed

    Prof.Dr. Zizheng GONG

    China Academy of Space Technology (CAST)

    China

    9

    11:51

    mass distribution and dependence on impact parameters of spacecraft breakup debris

    18'

    confirmed

    Mr. SHENGWEI LAN

    China Aerodynamics Research and Development Center (CARDC) 

    China

    10

    12:09

    Hyper velocity impact analysis of cube sat and subsequent orbit determination

    18'

    withdrawn

    Dr. Ugur Guven

    United States

    recent progresses of micro-space debris hypervelocity impact tests using laser-driven flyer techniques in CAST

    MERGED 29049

    confirmed

    Prof.Dr. Zizheng GONG

    China Academy of Space Technology (CAST)

    China