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  • IAC-23
  • A6
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  • session 3

    Title

    Impact-Induced Mission Effects and Risk Assessments

    type

    oral

    Description

    This session addresses disruptions of spacecraft operations induced by hypervelocity impacts including spacecraft anomalies, perturbation of operations, component failures up to mission loss , and spacecraft fragmentations. It includes risk assessments for impact vulnerability studies and corresponding system tools. Further topics are spacecraft impact protection and shielding studies, laboratory impact experiments, numerical simulations, and on-board diagnostics to characterize impacts such as impact sensors, accelerometers, etc.

    Date

    2023-10-04

    Time

    10:15

    Room

    BCC A6

    IPC members
    • Co-Chair: Prof. Zizheng Gong, Beijing Institute of Spacecraft Environment Engineering, China Academy of Space Technology (CAST), China;

    • Co-Chair: Dr. Yukihito Kitazawa, Japan Aerospace Exploration Agency (JAXA), Japan;

    • Rapporteur: Mr. Jean-Claude Traineau, Office National d’Etudes et de Recherches Aérospatiales (ONERA), France;

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    10:15

    KEYNOTE: Progress in China’s Space Debris Protection Research-Retrospect and Prospect

    24

    confirmed

    Prof. Zizheng Gong

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

    China

    2

    10:39

    Risk assessment of hypervelocity impact-induced electrical anomalies on spacecraft

    14

    confirmed

    Mr. Tayyar Shirinli

    Azercosmos, Space Agency of Republic of Azerbaijan

    Azerbaijan

    3

    10:53

    Investigation on shock Hugoniot of polyimide via all-atom molecular dynamics simulation

    14

    confirmed

    Dr. Tao Liu

    China

    4

    11:07

    An overview on Smart Ballistic Optimization for Repairing of Aerospace Exostructures using 3D printed Kevlar

    14

    confirmed

    Dr. Leonardo Barilaro

    Malta

    5

    11:21

    Simulating Impact-Induced Satellite Breakups with a Discrete Element Method

    14

    confirmed

    Mr. Noah Ledford

    Fraunhofer EMI

    Germany

    6

    11:35

    Investigation of aluminium Whipple Shield response to hypervelocity impacts close to ballistic limit between 2.5 and 5 km/s

    14

    confirmed

    Dr. Lorenzo Olivieri

    CISAS "G. Colombo" - University of Padova

    Italy

    7

    11:49

    Glancing impact on a picosatellite mock-up: test results

    14

    confirmed

    Dr. Lorenzo Olivieri

    CISAS "G. Colombo" - University of Padova

    Italy

    8

    12:03

    Projectile shape effect on fragment size distribution in a debris cloud produced by a hypervelocity impact onto thin aluminum plate

    14

    withdrawn

    Dr. Shengyu Zou

    China Aerodynamics Research and Development Center (CARDC) 

    China

    9

    12:17

    A study on the hazards of space debris for lunar missions: A review

    14

    confirmed

    Mr. Shreyansh Dubey

    University of Petroleum and Energy Studies

    India

    10

    12:31

    Hypervelocity impact characteristics of multilayer reactive material bumper shield against large size projectiles

    14

    confirmed

    Prof. Zizheng Gong

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

    China