session P

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

papers
Order	Paper title	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1	Commercialization of Space: Issues, Opportunities and Challenges for Active Debris Removal	withdrawn	Dr.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2	Numerical study on debris cloud behind Al/Mg wave impedance-grade bumper	withdrawn	Dr.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5	A system concept for the active space debris removal demonstration mission	withdrawn	Dr.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6	a spaceborne debris surveillance radar based on multistatic cross array	withdrawn	Mr.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7	Kinetic characteristics of satellites in tether drag deorbiting	withdrawn	Dr.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detection algorithm of small and fast orbital objects using faint streaks; application to geosynchronous orbit objects	withdrawn	Mr.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11	optical observation, image-processing, and detection of space debris in geosynchronous earth orbit	withdrawn	Dr.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14	Practical Particle Impact Risk Assessment in Satellite Projects	withdrawn	Mr.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

session P

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