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  • session 2

    Title

    Modeling and Risk Analysis

    Description

    This session will address the characterization of the current and future debris population and methods for in-orbit and on-ground risk assessments. The in-orbit analysis will cover collision risk estimates based on statistical population models and deterministic catalogs and active avoidance, including evasive manoeuvres.

    Date

    2009-10-13

    Time

    10:00

    Room

    Technical Session #17

    IPC members
    • Chairman: Prof.Dr. Heiner Klinkrad, European Space Agency (ESA), Germany;

    • Chairman: Dr. Vladimir Agapov, Keldysh Institute of Applied Mathematics, RAS, Russian Federation;

    • Rapporteur: Dr. Mark J. Matney, National Aeronautics and Space Administration (NASA), United States;

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    2

    GEOSYNCHROUS ENVIRONMENT FOR ORDEM2008

    15'

    Dr. Paula H. Krisko

    National Aeronautics and Space Administration (NASA)

    United States

    3

    The MASTER-2009 Fragmentation Model for the Small Size Regime

    15'

    Mr. Sven Kevin Flegel

    Technische Universität Braunschweig

    Germany

    5

    analysis for chain-crash risk of leo satellite due to collision between iridium-33 and cosmos-2251

    15'

    Mrs. Eun-Jung Choi

    Satrec Initiative

    Korea, Republic of

    6

    A New Space Debris Environment Model SDEM

    15'

    Prof. Shuang Li

    Nanjing University of Aeronautics and Astronautics

    China

    7

    NaK release model for MASTER-2009

    15'

    Dr. Carsten Wiedemann

    Technical University of Braunschweig

    Germany

    8

    Impact sensing systems and estimated impact rates of the upcoming Meteoroid and Space Debris Detector experiment (MDD3) onboard Russian Spektr-R satellite

    15'

    Dr. Frank Schäfer

    Fraunhofer EMI

    Germany

    9

    Improved Orbital Debris Trajectory Estimation Based on Sequential TLE Processing

    15'

    Ms. Alana Muldoon

    University of California

    United States

    10

    Success Rate and Effect of using Electrodynamic Tether System for De-orbit LEO Spacecraft

    15'

    Ms. Ieyoung Kim

    Kyushu University

    Japan