session P

Title: Poster Session
type: poster
Date: 2014-10-01
Time: 13:15
Room: Prefunction

papers
Order	Paper title	Presentation status	Speaker	Affiliation	Country
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
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
10	The CanX-7 Deorbit Mission: Demonstrating Deorbiting Technologies for Micro and Nanosatellites	confirmed	Mr. Thomas Sears	Space Flight Laboratory, University of Toronto	Canada
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
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
23	The impact of growing Space Debris on third-party-liability insurance	confirmed	Ms. Anja Nakarada Pecujlic	University of Vienna	Austria
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 (FGUP 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
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
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
43	Mitigating Orbital Debris in LEO with High Power Pulsed Laser		Mr. Alaa Hussein	University of Sussex	United Kingdom
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
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 (FGUP 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
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
65	Basic Experiment on Electromagnetic Irradiation Caused by Hypervelocity Impact	confirmed	Mr. Masakazu Kobayashi	Tokai University	Japan
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
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
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

session P

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