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  • session 3

    Title

    Impact-Induced Mission Effects and Risk Assessments

    Description

    This session addresses disruptions of spacecraft operations induced by hypervelocity impacts including spacecraft anomalies, perturbation of operations, and component failures up to mission loss. 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

    2018-10-03

    Time

    09:45

    Room

    ZARM 1

    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: Dr. Darren McKnight, Integrity Applications Incorporated (IAI), United States;

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    09:45

    experimental study on performances for the different graded-impedance distribution materials

    18

    confirmed

    Dr. Guangming Song

    China Academy of Space Technology (CAST)

    China

    2

    10:03

    Characteristics of Microwave Emissions from Hypervelocity Impacts on Pure Aluminum and Various Aluminum Alloy Plates

    18

    confirmed

    Mr. Yuki Mando

    The Graduate University for Advanced Studies

    Japan

    3

    10:21

    Orbital Debris Risk Assessment of Harnessing: Comparing Aluminum Plate Ballistic Limit Equation Predictions to Test Data

    18

    confirmed

    Mr. James Chinn

    Jet Propulsion Laboratory - California Institute of Technology

    United States

    4

    10:39

    Characterizing DebriSat Fragments -- Preliminary Results

    18

    confirmed

    Ms. Samantha Allen

    University of Florida

    United States

    5

    10:57

    Measuring impact craters on the ISS Columbus Module

    18

    confirmed

    Mr. Robin Putzar

    Fraunhofer EMI

    Germany

    6

    11:15

    Research on the Analysis Method of Failure Probability Caused by the Impact of Space Debris

    18

    confirmed

    Dr. Sen Liu

    China Aerodynamics Research and Development Center (CARDC) 

    China

    7

    11:33

    Experimental characterization of multi-layer 3D-printed shields for microsatellites

    18

    confirmed

    Dr. Lorenzo Olivieri

    CISAS "G. Colombo" - University of Padova

    Italy

    8

    11:51

    Cross-validation of the Meteoroid and Orbital Debris Risk and Damage Assessment Tools ESABASE2/Debris and BUMPER

    18

    confirmed

    Mr. Anatoli Miller

    Etamax Space GmbH

    Germany

    9

    12:09

    CST: a new semi-empirical tool for simulating spacecraft collisions in orbit

    18

    confirmed

    Prof. Alessandro Francesconi

    University of Padova - DII/CISAS

    Italy

    10

    12:27

    Modeling of the impact micrometeoroid and orbital debris on the Micrometeoroids and Debris Protection System for inflatable modules for lunar orbital application

    18

    confirmed

    Dr. Natalia Goldenko

    TSNIIMASH

    Russian Federation

    Enhanced Orbital Debris Shielding Structure With Impedance-Graded Materials

    confirmed

    Prof. Zizheng Gong

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

    China

    How to Effectively Map Space Debris Impact Crater Distribution and Morphology on Spacecraft Hulls

    Dr. Max Gulde

    Fraunhofer EMI

    Germany

    Performance Characteristics of DebriSat Imaging Systems

    Mr. Bungo Shiotani

    University of Florida

    United States