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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

    2014-10-01

    Time

    09:45

    Room

    801B

    IPC members
    • Co-Chair: Prof. Alessandro Francesconi, University of Padova - DII/CISAS, Italy;

    • Co-Chair: Dr. Sen Liu, China Aerodynamics Research and Development Center (CARDC) , China;

    • Rapporteur: Mr. Frank Schaefer, Fraunhofer - Institut für Kurzzeitdynamik, Ernst-Mach-Institut (EMI), Germany;

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    MMOD Impact Damage to ISS

    15'

    withdrawn

    Mr. James Hyde

    Barrios Technology/ESC Group - NASA

    United States

    2

    Measurement of micro-debris flux via TANPOPO capture panel onboard the ISS Kibo Exposed Facility

    15'

    confirmed

    Ms. Yuu Takayanagi

    Hosei University

    Japan

    3

    influences of impact position and angle on shielding performance of n-shape configuration

    15'

    confirmed

    Mr. Xuezhong Wen

    China Aerodynamics Research and Development Center (CARDC) 

    China

    4

    hypervelocity impact characteristics of basalt fiber woven/al-mesh combination bumper stuffed in whipple shield

    15'

    withdrawn

    Dr. Bin Jia

    Harbin Institute of Technology

    China

    5

    An engineering model to describe fragments clouds propagating inside spacecraft in consequence of space debris impact on sandwich panel structures

    15'

    confirmed

    Prof. Alessandro Francesconi

    University of Padova - DII/CISAS

    Italy

    6

    Determination of coordinates for a point of pressurized compartment puncture at collision with a high-speed particle

    15'

    withdrawn

    Dr. Vladimir Lapygin

    Central Research Institute for Machine Building (JSC TSNIIMASH)

    Russian Federation

    7

    EXPERIMENTAL VERIFICATION OF AN INNOVATIVE DEBRIS DETECTOR

    15'

    confirmed

    Mr. Waldemar Bauer

    Deutsches Zentrum für Luft- und Raumfahrt e.V. (DLR)

    Germany

    8

    The study of small space debris impact inducing discharge

    15'

    withdrawn

    Dr. Li Hongwei

    National Space Science Center (NSSC), Chinese Academy of Sciences

    China

    9

    Modeling of damage formation on a front wall of shielded composite overwrapped pressure vessel subjected to space debris impact

    15'

    confirmed

    Prof. Igor Telichev

    University of Manitoba

    Canada

    10

    Multi-shock shield performance at 15 MJ for catalogued debris

    15'

    withdrawn

    Dr. Joshua Miller

    National Aeronautics and Space Administration (NASA), Johnson Space Center

    United States

    11

    cardc-sbm spacecraft breakup model and its application

    15'

    confirmed

    Dr. Sen Liu

    China Aerodynamics Research and Development Center (CARDC) 

    China

    12

    A new method to predict the catastrophic disintegration of spacecraft upon collision with large orbital debris

    15'

    confirmed

    Dr. Mirco Zaccariotto

    University of Padova, DII / CISAS – “G. Colombo”

    Italy