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  • session 3

    Title

    Hypervelocity Impacts and Protection

    type

    oral

    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

    2017-09-27

    Time

    09:45

    Room

    Hall E1

    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

    Review of MMOD Shielding of the Chinese Space Station

    18

    confirmed

    Dr. Jun Yan

    China Academy of Space Technology (CAST)

    China

    2

    Predicting the Consequences of Micrometeoroid and Orbital Debris Penetrations on the International Space Station

    18

    withdrawn

    Mr. James Hyde

    Barrios Technology/ESC Group - NASA

    United States

    3

    hypervelocity impact damage pattern recognition in aluminum alloy plates based on d-s evidence theory and bp neural network

    18

    Dr. cao wuxiong

    School of Astronautics, Harbin Institute of Technology

    China

    4

    Study on the performance of shielding configuration for reducing the fixing weight of fiber layer

    18

    confirmed

    Mr. Fa-wei Ke

    China Aerodynamics Research and Development Center (CARDC) 

    China

    5

    The influence of mechanical laminate properties on the hypervelocity impact resistance of Fiber Metal Laminates

    18

    withdrawn

    Mr. Chunsen Shi

    Delft University of Technology (TU Delft)

    The Netherlands

    6

    Characterizing DebriSat Fragments: So many fragments, so much data, and so little time

    18

    confirmed

    Mr. Bungo Shiotani

    University of Florida

    United States

    7

    Optical Fragment Tracking in Hypervelocity Impact Experiments

    18

    confirmed

    Mr. Erkai Watson

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

    Germany

    8

    Experimental investigation on the damage characteristic of solar array under millimeter size orbital debris hypervelocity impact

    18

    confirmed

    Prof. Zizheng GONG

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

    China

    9

    Microwave Emission from Hypervelocity Impacts Using Aluminum and Nylon for Target and Projectile Materials

    18

    confirmed

    Mr. Yuki Mando

    The Graduate University for Advanced Studies

    Japan

    10

    Spacecraft Debris Generation due to Materials Degradation for LEO Orbit Conditions

    18

    withdrawn

    Mr. Paulo Gordo

    Faculdade de Ciências da Universidade de Lisboa

    Portugal

    Risk assessment of sustained discharge on satellite’s power harnesses caused by space debris impacts

    withdrawn

    Dr. Takayuki Hirai

    Japan Aerospace Exploration Agency (JAXA)

    Japan