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  • session P

    Title

    Poster Session

    type

    poster

    Date

    2014-10-01

    Time

    13:15

    Room

    Prefunction

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    Commercialization of Space: Issues, Opportunities and Challenges for Active Debris Removal

    withdrawn

    Dr. Rushi Ghadawala

    Aryavarta Space Organization

    India

    2

    Numerical study on debris cloud behind Al/Mg wave impedance-grade bumper

    withdrawn

    Dr. Mingqiang Hou

    China

    3

    study on space debris mitigation mechanism

    Ms. Li Chai

    The Academy of Equipment

    China

    4

    A High-Precision DF Method with Double Station based on Phase-Differential Measure

    Prof. Yu tao

    The 51 st Research Institute of CETC

    China

    5

    A system concept for the active space debris removal demonstration mission

    withdrawn

    Dr. Lihua Zhang

    DFH Satellite Co. Ltd.

    China

    6

    a spaceborne debris surveillance radar based on multistatic cross array

    withdrawn

    Mr. Wei Xiang

    China

    7

    Kinetic characteristics of satellites in tether drag deorbiting

    withdrawn

    Dr. Guowei Zhao

    Beihang University

    China

    8

    a conjunction risk assessment method for F-value based on two-line elements

    confirmed

    Mr. Chaowei Ma

    Beijing Institute of Tracking and Telecommunication Technology (BITTT)

    China

    9

    detection algorithm of small and fast orbital objects using faint streaks; application to geosynchronous orbit objects

    withdrawn

    Mr. Makoto Tagawa

    Kyushu University

    Japan

    10

    The CanX-7 Deorbit Mission: Demonstrating Deorbiting Technologies for Micro and Nanosatellites

    confirmed

    Mr. Thomas Sears

    Space Flight Laboratory, University of Toronto

    Canada

    11

    optical observation, image-processing, and detection of space debris in geosynchronous earth orbit

    withdrawn

    Dr. Hiroshi ODA

    Japan Aerospace Exploration Agency (JAXA)

    Japan

    12

    relative determination for non-cooperative spacecraft based on binocular vision system

    confirmed

    Mr. Cai Han

    China

    13

    Analysis of Space Debris and slow down it's velocity

    Mr. Sourabh Kaushal

    Engineer

    India

    14

    Practical Particle Impact Risk Assessment in Satellite Projects

    withdrawn

    Mr. Jan-Christian Meyer

    OHB System AG-Bremen

    Germany

    15

    Collision probability assessment for Active Debris Removal missions

    confirmed

    Mr. Aleksander Lidtke

    University of Southampton

    United Kingdom

    16

    meteoroid stream modelling using distributed computing to define the impact hazard to spacecraft caused by natural space debris

    confirmed

    Mr. Maximilian Sommer

    University of Stuttgart

    Germany

    17

    Performance Mapping of Space Debris Removal Concepts

    confirmed

    Mr. Seyed Ali Nasseri

    Space Generation Advisory Council (SGAC)

    Canada

    18

    studies of the mechanical properties of self-healing composites in a space environment

    confirmed

    Mr. Mehdi Sabzalian

    Concordia University

    Canada

    19

    Multi-target Tracking Management for a Multifunctional Radar in Space Situational Awareness

    confirmed

    Dr. Hai Jiang

    National Astronomical Observatories, Chinese Academy of Sciences

    China

    20

    Behavior of ejectors at oblique collision for developing a debris shield

    confirmed

    Ms. Hiroka Hamatani

    Kogakuin University

    Japan

    21

    RISKS OF COLLISION OF LAUNCH VEHICLES WITH THE CATALOGUED SPACE OBJECTS IN THE ASCENT PHASE

    Mr. Alexandr Golubek

    Yuzhnoye State Design Office

    Ukraine

    22

    research on charging effect of small & medium-sized space debris in ionosphere plasma environment

    withdrawn

    Dr. Weijie Wang

    Academy of Equipment

    China

    23

    The impact of growing Space Debris on third-party-liability insurance

    confirmed

    Ms. Anja Nakarada Pecujlic

    University of Vienna

    Austria

    24

    Study of a harpoon with a foam injection system for debris mitigation.

    withdrawn

    Mr. Idriss Sisaid

    Cranfield University

    France

    25

    Space Debris: Lessons learned from the marine environment

    withdrawn

    Ms. Rose Tasker

    Australia

    26

    Robotic Arm To Clean Space Debris

    withdrawn

    Mr. Naman Vaidya

    Manipal Institute of Technology, Manipal University

    India

    27

    a collaborative approach to space debris mitigation using de-orbit kit technology

    Mr. Jean-Pierre Coadou

    Nova Shell Materials Technologies

    Canada

    28

    Self-contained onboard LV stage disposal system based on energy resources unexpended after SC orbital insertion

    confirmed

    Dr. Yakov Shatrov

    Central Research Institute for Machine Building (JSC TSNIIMASH)

    Russian Federation

    29

    LIQUID PROPELLANT BEHAVIOUR PECULIARITIES UNDER THEIR DISCHARGE IN VACUUM FROM TANKS DURING PASSIVATION OF THE LV WASTED STAGES

    confirmed

    Mr. Anatolii Lohvynenko

    Yuzhnoye State Design Office

    Ukraine

    30

    Ariane 4 H10 target orbital thermal analysis and IR recognition

    withdrawn

    Dr. Ciro Borriello

    Aviospace S.R.L

    Italy

    31

    Continuity equation approach for the analysis of the collision risk due space debris clouds generated by a fragmentation event

    confirmed

    Ms. Francesca Letizia

    University of Southampton

    United Kingdom

    32

    SOME DESIGN APPROACHES TO PREVENT AND LIMIT THE NEAR-EARTH SPACE DEBDIS GENERATION

    confirmed

    Mr. Gennadiy Osinovyy

    Yuzhnoye State Design Office

    Ukraine

    33

    numerical simulation on the shielding configurations with middle layer of corrugation and honeycomb cone respectively

    confirmed

    Mr. Fa-wei Ke

    China Aerodynamics Research and Development Center (CARDC) 

    China

    34

    Using MLIs as Hypervelocity impact mitigation: An unintended test in orbit.

    withdrawn

    Mr. Ronnie Nader

    Ecuadorian Civilian Space Agency (EXA)

    Ecuador

    35

    Identifying Origin of Breakup Event by In-situ Measurement

    confirmed

    Mr. Mitsuhiko Tasaki

    Kyushu University

    Japan

    36

    An analytical method for the propagation towards internal components of debris clouds originated by space debris impacts on spacecraft walls

    confirmed

    Prof. Alessandro Francesconi

    University of Padova - DII/CISAS

    Italy

    37

    Real-time Determination Method for Telescope Pointing Error

    confirmed

    Dr. Xiaoxiang Zhang

    China

    38

    new method of echo detection for diffuse reflection laser ranging of space debris

    Dr. Kunpeng Wang

    China

    39

    Methodological approach to the problem of on-time identification of space debris with the use of spacecraft onboard optical sensors

    confirmed

    Mr. Nikolay Panichkin

    Central Research Institute of Machine Building (FSUE/TSNIIMASH)

    Russian Federation

    40

    Securing future Earth-Moon commercial space travels: simulation of capture and de-orbit phases for active debris removal in near-Earth orbits

    confirmed

    Ms. Melissa Zemoura

    Kyushu University

    Japan

    41

    Mission Concept for Multi Space Debris Removal

    confirmed

    Mrs. Susanne Peters

    Universität der Bundeswehr München

    Germany

    42

    The Dynamics of Tethered Debris With Flexible Appendages and Residual Fuel

    withdrawn

    Prof. Vladimir S. Aslanov

    Samara National Research University (Samara University)

    Russian Federation

    43

    Mitigating Orbital Debris in LEO with High Power Pulsed Laser

    Mr. Alaa Hussein

    University of Sussex

    United Kingdom

    44

    Recycling Space Junk: Resource Harvesting as a Solution for Orbital Debris

    withdrawn

    Ms. Zahra Khan

    Massachusetts Institute of Technology (MIT)

    United States

    45

    Launch Adapter Ring Capture Tool: Canadian Robotic Technology for the Autonomous Capture of Unprepared and Non-Operational Debris

    confirmed

    Mr. Richard Rembala

    MDA Space Missions

    Canada

    46

    Estimation of Inertia Parameters of a Space Debris for Its Tether-Assisted Removal

    withdrawn

    Mrs. Fan Zhang

    McGill University

    Canada

    47

    The last results of activity Russian Federation in fields of modeling space debris and mitigation measures in near Earth space

    confirmed

    Mr. Igor Usovik

    Central Research Institute for Machine Building (JSC TSNIIMASH)

    Russian Federation

    48

    Deriving a priority list based on the environmental criticality

    confirmed

    Mr. Christopher Kebschull

    Technische Universität Braunschweig

    Germany

    49

    Effects of temperature of targets on ejecta size distribution in hypervelocity impact

    confirmed

    Dr. Masahiro Nishida

    Nagoya Institute of Technology

    Japan

    50

    Improvement of the two-stage light-gas accelerators performance by using the Photonic Doppler Velocimetry (PDV)

    confirmed

    Mr. Jan Hupfer

    Fraunhofer EMI

    Germany

    51

    market for high precision debris data

    confirmed

    Dr. Eugene Levin

    Electrodynamic Technologies, LLC

    United States

    52

    Can Pulsed Laser Ablation Prevent Most Debris Creation?

    confirmed

    Mr. Joseph Carroll

    Tether Applications, Inc.

    United States

    53

    Development and in-orbit verification of deployable sail structures for debris mitigation with a cubesat

    confirmed

    Mr. Engelbert Plescher

    FH Aachen University of Applied Sciences

    Germany

    54

    Collisions Probabilities and Mitigations Strategies of the QB50 Network

    confirmed

    Mr. Diederik Florijn

    Delft University of Technology (TUD)

    The Netherlands

    55

    sizing of an electrodynamic tether to deorbit debris in low earth orbit

    confirmed

    Mr. Antoine ARVEILLER

    ESTACA

    French Guiana

    56

    A Quick Method of Forecasting of Conflicting Approaches of Orbital Objects and Calculation of Parameters of an Approach

    Ms. Tatyana V. Labutkina

    Dnepropetrovsk National University named after Oles' Gonchar

    Ukraine

    57

    Additional Orbital Fragmentation Events

    confirmed

    Dr. Carsten Wiedemann

    Technical University of Braunschweig

    Germany

    58

    Active Debris Removal: Consequences of Mission Failure

    confirmed

    Dr. Hugh G. Lewis

    University of Southampton

    United Kingdom

    59

    Modeling dynamics of tethered small satellite for de-orbiting

    confirmed

    Mr. Shantanu Shahane

    Indian Institute of Technology

    India

    60

    The influence of the Relative Angular Velocity between Space-based Optical Detector and Space Debris in Detectable Analysis

    withdrawn

    Ms. Jingjing Hu

    University of Chinese Academy of Sciences;National Astronomical Observatories, Chinese Academy of Sciences

    China

    61

    design of a flexible satellite system for the mitigation of large sized orbital debris

    confirmed

    Mr. Christopher Gover

    Carleton Univeristy

    Canada

    62

    Numerical study on debris cloud behind Al/Mg wave impedance-grade bumper

    confirmed

    Prof.Dr. Zizheng GONG

    China Academy of Space Technology (CAST)

    China

    63

    Overview of Orbital Debris Mitigation Technologies

    confirmed

    Mr. Phil Smith

    Bryce Space and Technology

    United States

    64

    space debris removal using ecological missions

    withdrawn

    Mr. Logesh Sadasivam

    SRM University, kattankulathur,chennai,INDIA

    India

    65

    Basic Experiment on Electromagnetic Irradiation Caused by Hypervelocity Impact

    confirmed

    Mr. Masakazu Kobayashi

    Tokai University

    Japan

    66

    the research of residual fuel estimation and drain judge method in satellite end-of-life disposal

    withdrawn

    Mr. LUO LIANG

    China

    67

    study on debris shield stuffed with aerogel/fiberglass composite

    confirmed

    Mr. Xuezhong Wen

    China Aerodynamics Research and Development Center (CARDC) 

    China

    68

    Detection and Tracking of Debris using Space-borne Platforms

    confirmed

    Prof. Andrew Dempster

    University of New South Wales

    Australia

    69

    angle-only data acquisition from optical observation campaign to set an effective tracking strategy of geo object, coms 1 of korea

    confirmed

    Mr. Jin Choi

    University of Science & Technology

    Korea, Republic of

    70

    Optical technologies for observation of low earth orbit objects

    confirmed

    Dr. Daniel Hampf

    German Aerospace Center (DLR)

    Germany

    71

    Motion and Control of Debris Capture with Super Multi-link Space Manipulator

    confirmed

    Mr. Yoshito TSUJIMOTO

    Yokohama National University

    Japan

    72

    SPACE DEBRIS AND ASTEROIDS DETECTION FROM TOPPO DI CASTELGRANDE OBSERVATORY

    confirmed

    Dr. Vladimir Agapov

    Keldysh Institute of Applied Mathematics, RAS

    Russian Federation

    73

    the effect of specular reflectance on space target detecting

    Dr. DEXIAN ZENG

    Academy of Equipment

    China

    74

    survey and origin identification of breakup debris using time delay integration method

    confirmed

    Mr. Yuki SETO

    Kyushu University

    Japan

    75

    integrated analysis of space environment effects on space-based visible camera

    confirmed

    Dr. DEXIAN ZENG

    Academy of Equipment

    China

    76

    Space Debris Remediation Using Solutions for On-Orbit Servicing

    confirmed

    Dr. Peter Hofmann

    OHB System AG - Munich

    Germany

    77

    design and analysis of a drag sail to de-orbit low earth orbit satellites

    confirmed

    Mr. Mir Mohammad Furqan

    Siddaganga Institute of Technology

    India

    78

    Automatic object tracking for Space based space debris observation

    confirmed

    Mr. Francesco Diprima

    Italy

    79

    orbit determination from space-based optical observation

    confirmed

    Dr. Gioacchino Scire

    Italy

    80

    Mitigation of Space Debris From MEO Using Solar Sail with Performance Index of Energy Consumption and Weight as the Two Objectives for Optimization

    withdrawn

    Ms. Assal Soumekh

    Amirkabir University of Technology

    Iran

    81

    LEO Space Debris Mitigation Using Laser Ablation

    confirmed

    Mr. Alaa Hussein

    University of Sussex

    United Kingdom

    82

    Deployable Drag Device for Launch Vehicle Upper Stage De-Orbit

    confirmed

    Ms. Alexandra Long

    School of Aerospace Engineering, Georgia Institute of Technology

    United States

    83

    De-orbiting Uncooperative Bodies for Debris Mitigation

    withdrawn

    Dr. Steve Jolly

    Lockheed Martin (Space Systems Company)

    United States

    84

    Ground-based Optical Observation System for LEO Objects

    confirmed

    Dr. Toshifumi Yanagisawa

    Japan Aerospace Exploration Agency (JAXA)

    Japan

    Control scheme of tether drag deorbit system in orbital plane

    confirmed

    Dr. Liang Sun

    Beihang University

    China