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  • session 5

    Title

    Space Debris Removal Issues

    Description

    This session will address active removal techniques "ground and space based", review potential solutions and identify implementation difficulties.

    Date

    2017-09-28

    Time

    09:45

    Room

    Hall E1

    IPC members
    • Co-Chair: Mr. Benjamin Bastida Virgili, European Space Agency (ESA), Germany;

    • Co-Chair: Prof. Fabio Santoni, Sapienza University of Rome, Italy;

    • Rapporteur: Dr. Fabrizio Piergentili, Sapienza University of Rome, Italy;

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    End-to-end On Ground System Demonstration of combined technologies for Debris Removal applications

    15

    confirmed

    Mr. Pablo Colmenarejo

    GMV Aerospace & Defence SAU

    Spain

    2

    A Passively Stable Pyramid Sail for the Deorbit of Small Satellite Constellations

    15

    confirmed

    Ms. Alexandra Long

    School of Aerospace Engineering, Georgia Institute of Technology

    United States

    3

    Standardized passive deorbiting device for multiple cubesat class SC: from 1U to 12U

    15

    confirmed

    Mr. Niccolò Bellini

    N.P.C. New Production Concept

    Italy

    4

    development of a solid rocket motor for an active deorbitation system

    15

    confirmed

    Mr. Michal Pakosz

    Institute of Aviation

    Poland

    5

    laboratory demonstration of space debris removal by a bi-directional helicon plasma thruster

    15

    confirmed

    Dr. Kazunori Takahashi

    Tohoku University

    Japan

    6

    Contact Dynamics of Net Capturing of Space Debris

    15

    confirmed

    Mr. Minghe Shan

    Delft University of Technology (TU Delft)

    The Netherlands

    7

    Trajectory Tracking and Stability Control of the Space Net Robot for Reconfiguration

    15

    withdrawn

    Mrs. Fan Zhang

    Northwestern Polytechnical University

    China

    8

    comparison of efficiency of two de-orbiting schemes for adr mission in leo

    15

    confirmed

    Mr. Dmitriy Grishko

    Bauman Moscow State Technical University

    Russian Federation

    9

    Low thrust trajectory optimization for multiple space debris removal

    15

    confirmed

    Mr. Xun Pan

    Northwestern Polytechnical University,NPU

    China

    10

    Taxonomy and Analysis of Issues Facing Post Mission Disposal Concepts

    15

    confirmed

    Ms. Emma Kerr

    University of Strathclyde

    United Kingdom

    11

    Increased Debris Cloud Density Due to Precession of Argument of Perigee

    15

    confirmed

    Dr. Joel Slotten

    United States