session IP

Title: Interactive Presentations
Date: 2015-10-14
Time: 13:15

IPC members

Coordinator: Dr. Constantinos P. Stavrinidis, IABG Industrieanlagen - Betriebsgesellschaft mbH, Germany;
Coordinator: Prof. Pavel M. Trivailo, RMIT University, Australia, Australia;

papers
Order	Paper title	Presentation status	Speaker	Affiliation	Country
1	Dynamics Analysis of Flexible Cone Undergoing Space Docking		Dr. wei han	National University of Defense Technology	China
2	Ka Band Metal Wire Mesh Development for Deployable Reflector	withdrawn	Dr. XiaoFei Ma	Xi’an Institute of Space Radio Technology	China
3	A new multi-layer and graded-density flexible ablator		Ms. Luo Lijuan		China
4	research on the frequency characterization method of structural design	confirmed	Dr. Linan SHI	Science and Technology on Space Physics Laboratory	China
5	Research on Active Flutter Suppression Using Robustic Control Methodology for Reusable Launch Vehicle	confirmed	Mr. Junpeng Hui	China Academy of Launch Vehicle Technology (CALT)	China
6	aerodynamic design of a lifting re-entry vehicle for real gas effect flight test	confirmed	Mr. Bingyan Chen	China Academy of Aerospace Aerodynamics (CAAA)	China
7	Transfer Path Analysis of Dynamic Loading for the Second stage Liquid Rocket Engine		Dr. Binchao Li	Xi'an Aerospace Propulsion Institute	China
8	The influence factor of the dispersibility of carbon nano tube in epoxy resin		Mr. zhou fang	China Academy of Launch Vehicle Technology(CALT)	China
9	Effect of Rectangular Nozzle Water-Cooling Wall on the Total Enthalpy Loss of High Temperature Airflow in Arc-Heated Wind Tunnel	withdrawn	Mr. Jinlong Peng	China Academy of Aerospace Aerodynamics (CAAA)	China
10	dynamic properties study and optimization of astronautic separation products with different extension and compression stiffness	withdrawn	Dr. Shao-wei Feng	China Academy of Launch Vehicle Technology (CALT)	China
11	Studies on Aero Thermodynamics performance of the rudder with Zero Sweepback in Arc Heated Tunnel		Mr. Kao XU	China Academy of Aerospace Aerodynamics (CAAA)	China
12	Design and optimization of flat type loop heat pipe with multiple parallel evaporators	confirmed	Mr. Xiaoyu Zhang	China Academy of Launch Vehicle Technology(CALT)	China
13	a new approach based on metallographic analysis and micro Hardness test on evaluating the temperature of reusable ramjet engine	confirmed	Mr. ren jiawan		China
14	structural design and topology optimization of a university micro-satellite		Ms. Jing Guo	School of Astronautics, Beihang University	China
15	an immersed boundary method for compressible flow simulation	confirmed	Mr. YueLong He	China Academy of Aerospace Aerodynamics (CAAA)	China
16	Study on Satellite segment vibration test technology	withdrawn	Mr. Hao Jiang		China
17	Study on thermal protection materials ablation resulting in changes of flow field parameters in supersonic turbulent duct on arc heater	confirmed	Mr. you-hua zhang	China Academy of Aerospace Aerodynamics (CAAA)	China
18	Experimental study of low density thermal insulation materials on radiation heating facility with variable pressure	confirmed	Mr. lian-zhong chen	China Academy of Aerospace Aerodynamics (CAAA)	China
19	The establishment of dynamic model for the single-phase fluid loop system		Mr. Fanjian Zeng		China
20	Experimental Investigation on the Decomposition Rate of Phenolic Resin Thermal Protection Material	confirmed	Mr. Jian-qiang Tu	China Academy of Aerospace Aerodynamics (CAAA)	China
21	CVD methods for graphene generation on stainless steels for corrosion resistance	withdrawn	Mr. Michael Eisfelder	Monash University	Australia
22	Aerodynamic force and heat fast prediction for high speed vehicles based on effective numerical and engineering methods	confirmed	Mr. rong wang		China
23	A Study of Compressibility Corrections for k-omega SST Turbulence Model in Hypersonic Flow Applications	confirmed	Mr. Guo-hao DING	China Aerodynamics Research and Development Center (CARDC)	China
24	Experimental study on the thermal control device using the solid-liquid phase change material	confirmed	Prof. Taig Young Kim	Korea Polytechnic University	Korea, Republic of
25	Structural analysis of a critical deviation observed at an Interface in a Solid Rocket booster Motor using strain based acceptance criteria	confirmed	Mr. Paul Murugan J	Indian Space Research Organization (ISRO)	India
26	A study on the start-up, blocking-up and operating characteristics of loop heat pipe	confirmed	Dr. Dong La	Shanghai Institute of Satellite Engineering	China
27	REACTION CONTROL OF FLEXIBLE JOINT SPACE MANIPULATORS		Dr. Silvio Cocuzza	CISAS – “G. Colombo” Center of Studies and Activities for Space, University of Padova	Italy
28	Time-variant Reliability Analysis of Cabin's Door Considering Component Damage	confirmed	Dr. lin ye		China
29	Verification with quasi-static tests of composite structures for launchers, satellite and re-entry vehicles	confirmed	Dr. Davide Santachiara	DTM srl	Italy
30	Design and verification of high pressure high purity gas delivery systems for International Space Station	confirmed	Dr. Davide Santachiara	DTM srl	Italy
31	Investigation of Cabin Pressure Prediction for Intake and Exhaust System on Re-entry Vehicles		Mrs. Huiling Zhan	China Academy of Aerospace Aerodynamics (CAAA)	China
32	A rapid method to calculate the viscous force based on local inviscid flow field parameters	withdrawn	Mr. Gong Anlong		China
33	Numerical and experimental activities to assess the compatibility of the IXV mock-up custom avionic systems with the splash down shock loads.	confirmed	Dr. Vito Salvatore	CIRA Italian Aerospace Research Center, Capua	Italy
34	DESIGNING A STRUCTURE, ANTENNA AND SOLAR PANELS DEPLOYMENT SYSTEM FOR A STUDENT NANO SATELLITE BUS MODULE (NIUSAT MARK-I)	confirmed	Mr. Subash Chandran Selvan Nambi	Noorul Islam University, Noorul Islam Centre for Higher Education	India
35	epoxy based shape memory polymers for space applications	confirmed	Ms. Debby Margoy	SOREQ NRC	Israel
36	Research Development of Thermal Protection Material in High Enthalpy Thermal Environment for Lunar Return Reentry	withdrawn	Dr. HE GAO	China Academy of Aerospace Aerodynamics (CAAA)	China
37	cnt-polyimide nanocomposites for space applications	confirmed	Mrs. Nurit Atar	SOREQ NRC	Israel
38	Dynamic characteristic analysis of a moment control unit with vibration isolation capability and its application		Dr. Yao Zhang	Beijing Institute of technology(BIT)	China
39	Application of RANS/LES in Computing Hypersonic Turbulent Base Heating	confirmed	Mr. Xingliang Sun	Beihang University (BUAA)	China
40	The Design and Testing of Deployment Mechanisms and Structure of Twin Nano-Satellite, STUDSAT-2.	confirmed	Mr. Nikhilesh K V	NMAMIT NITTE	India
41	Reduction of processing time and human factor effects during the strength assessment of the spacecraft structure	confirmed	Mr. Nikolay Asmolovskiy	Space Structures GmbH	Germany
42	research on repeatable locking mechanism for space solar array	withdrawn	Mr. Lei Jia	China Academy of Launch Vehicle Technology(CALT)	China
43	Fold-Deployment Concept and Prototype Design for Air-Inflatable Solar Sail	confirmed	Ms. ZhengAi Cheng	Qian Xuesen Laboratory of Space Technology	China
44	Optimization of the cabin thermal environment control in a spacecraft on the ground preparation stage before launch	withdrawn	Dr. Qun Yu	China Academy of Launch Vehicle Technology (CALT)	China
45	Design Aspects of Head End Mounted Safe Arm (HMSA) for Igniters of Solid Rocket Motors	confirmed	Mr. Thomas Kurian	Indian Space Research Organization (ISRO)	India
46	Mechanism and kinetic characterization of the electron irradiation induced degradation of DGEBA/DICY		Dr. gang liu	China Academy of Space Technology (CAST)	China
47	Development and Study of Micro-Vibration Simulation Analysis System for Small Satellites	confirmed	Dr. Zhi Yang	DFH Satellite Co. Ltd.	China
48	Surface Figure Precision Analysis Research on Non-ideal Thin Film Solar Cells of Space Solar Power Satellite	confirmed	Dr. Chen Yang	Qian Xuesen Laboratory of Space Technology	China
49	shape optimization of inside-hole in triangular ribbed plate	confirmed	Ms. Yiqian Zhou		China
50	A Boundary Element Method for Transient Nonlinear Radiative-Conductive Coupled Heat Transfer Problems	confirmed	Dr. wang jing	CASC	China
51	on the development of arc tunnel test technology for control surface seal evaluations	confirmed	Mr. zhang qian	China Academy of Aerospace Aerodynamics (CAAA)	China
52	NOVEL IDENTIFICATION METHOD OF THE DYNAMIC PARAMETERS OF A SPACE MANIPULATOR		Dr. Silvio Cocuzza	CISAS – “G. Colombo” Center of Studies and Activities for Space, University of Padova	Italy

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