session IP

Title: Interactive Presentations
Description: This session offers a unique opportunity to deliver your key messages in an interactive presentation on any of the subjects of Materials and Structures addressed in the classic Sessions. The presentation will be displayed on a digital screen in a dedicated location and available for view by all Congress attendees for the entire Congress week. In addition, one afternoon is dedicated exclusively for the attendees to view the Interactive Presentations, and the author will be assigned a specific eight minute slot to personally present the topic and interact with the attendees present. The Interactive Presentation may take advantage of all electronic display capabilities, such as: PowerPoint charts, embedded hot links, pictures, audio and video clips etc. An award will also be presented to the author of the best Interactive Presentation in the C Category at a special ceremony. An Abstract that follows the standard format must be submitted by the deadline for standard IAC abstracts.
Date: 2017-09-28
Time: 12:45
Room: Hall J&K2

IPC members

Co-Chair: Prof. Paolo Gasbarri, University of Rome “La Sapienza”, Italy;
Co-Chair: Dr. Andreas Rittweger, DLR (German Aerospace Center), Germany;

papers
Order	Paper title	Presentation status	Speaker	Affiliation	Country
1	A brief discussion about force control of robot manipulators	withdrawn	Mr. Vinicius Piro Barragam	ITA-DCTA	Brazil
2	Synthesis and Characterization of Pr(3-x)Te(4) and Nd(3-x)Te(4) for High Temperature Thermoelectric Applications	withdrawn	Mr. Dean Cheikh	University of California, Los Angeles (UCLA)	United States
3	Analysis of type II and type III solar radio bursts using the e - CALLISTO system	withdrawn	Mr. Jude Wijesekera		Sri Lanka
4	Additive Manufactured Aerospike Reaction Control System	withdrawn	Mr. Eamon Hughes		United States
5	evaluation of end-of-life performance of gaas solar cell in gto mission using ion thruster		Dr. Xin Gao	Science and Technology on Vacuum Technology and Physics Laboratory, Lanzhou Institute of Physics	China
6	Water-Cooled Adjustable Material Probe Design for the Evaluation of Transient Heat Fluxes of High Temperature Materials	confirmed	Mr. Nicholas Harmansa	IRS, University of Stuttgart	Germany
7	Research on buffer mechanism and impact dynamics of pre-folded metal honeycomb structure	confirmed	Dr. Na Yao	Qian Xuesen Laboratory of Space Technology, China Academy of Space Technology (CAST)	China
8	a new approach for the environmental adaptability design, analysis and verification of a large spacecraft	withdrawn	Dr. Xinyu Zhang	Beijing Institute of Aerospace Systems Engineering, China Aerospace Science and Technology Corporation (CASC)	China
9	flight results of structure subsystem for enhanced epsilon launch vehicle	withdrawn	Mr. Hiroshi Ikaida	Japan Aerospace Exploration Agency (JAXA)	Japan
10	Ground and stratospheric flight tests on curing of composite materials in free space environment	confirmed	Prof. Alexey Kondyurin	The University of Sydney	Australia
11	Investigation of Co-Sn-Te Phase Space for Advancement of Skutterudite Materials for Radioisotope Thermoelectric Generators	confirmed	Ms. Caitlin Crawford	Colorado School of Mines, NASA Harriett G. Jenkins Fellow	United States
12	Energetic Composite Solid Propellants for advanced space systems	confirmed	Mr. vinayak malhotra	SRM University Chennai	India
13	Honeycomb Propellant Tank Design used for SRMSAT - 2	withdrawn	Mr. Subham Gupta	SRM University, kattankulathur, chennai, INDIA	India
14	Dimensional stability investigation of low CTE materials at temperatures from 140 K to 250 K using a heterodyne interferometer	confirmed	Ms. Ines Hamann	DLR (German Aerospace Center)	Germany
15	Characterization of Direct Metal Laser Sintered Impinging Injectors: Like-Doublet, Unlike Triplet, Like Quadlet, Unlike Pentad	confirmed	Mr. Deepak Atyam	Purdue University	United States
16	The Research of the Integrated Compound Insulator’s Strain Field Measurement under Bending Deformation based on Digital Image Correlation Method		Mr. Qiang Xiong	Beijing Aerospace Technology Institute	China
17	Analysis and Verification of Bearing Capacity of Stiffened Panel of Carbon Fiber Reinforced Polymer Composites	confirmed	Mr. CUI Shenshan	China Academy of Launch Vehicle Technology (CALT)	China
18	Problems of Modelling in dynamics of stabilization and orientation systems	confirmed	Prof. Lyudmila Kuzmina	Kazan National Research Technical University	Russian Federation
19	optimization of cylindrical composite material grid structure	withdrawn	Mr. Ilan Weissberg	Israel Aerospace Industries Ltd.	Israel
20	Characterization of Porosity via MicroCT for Selectively Laser Melted Titanium-64 and Inconel 718	withdrawn	Mr. Alexander Finch	Purdue University	United States
21	The study on materials thermal properties and optimal design for solar probe thermal protection	withdrawn	Prof. Oleg Alifanov	Moscow Aviation Institute	Russian Federation
22	A Multidisciplinary Software Chain for Integrated Structural, Thermal and Optical Performance Analysis of Space Instruments	confirmed	Dr. Stefan Bedrich	OHB System AG - Munich	Germany
23	Model Updating of Thermo-Elastic Plates of Spacecrafts in the Hot and Cold Space Environments	confirmed	Dr. He Liao		China
24	Testing and modeling for the creep and recovery behavior of Kevlar cables	confirmed	Prof. Tuanjie Li	Xidian University	China
25	Structural Dynamic Modification for Shock Response Spectra Test of a Fixture Based on Sensitivity Analysis of Anti-resonance Frequency	confirmed	Dr. DENG Changhua	Xi'an Aerospace Propulsion Institute	China
26	Revealer1601-RH : A radiation hardened NoC-based Multicore Digital Signal Processor	withdrawn	Dr. Hui Cao	Xi'an Microelectronics Technology Institute, China Academy of Space Electronics Technology (CASET), China Aerospace Science and Technology Corporation (CASC)	China
27	Paraffin-graphene/metal foam composite for thermal management in electronics	confirmed	Dr. Adriana Balan	University of Bucharest (UB)	Romania
28	Experimental Studies on Supersonic Aerothermal Fluid-Structure Interaction	confirmed	Mr. Dennis Daub	DLR (German Aerospace Center)	Germany
29	application of composite sandwich structure with lattice cores in aircraft lightening design	confirmed	Mr. zhenping zhao	CALT,CASC	China
30	A new type of electro-hydraulic complex servo actuator and its algorithm research based on launch vehicle		Dr. zhongliang zhang	Shanghai Aerospace Control Technology Institute (SACTI), Shanghai Academy of Spaceflight Technology (SAST)	China
31	A Fully Configurable Mass Dummy Design for Changing Spacecraft Structures	confirmed	Mr. Mehdi Sabzalian	Space Flight Laboratory, University of Toronto	Canada
32	The prospect of additive manufacturing in primary structure of launch vehicle	confirmed	Dr. Ji Bin	Aerospace System Engineering Shanghai, China	China
33	experiments on residual compressive strength after fatigue of cabon fiber fabric composites of spacecraft in hydrothermal environment	confirmed	Dr. xuan sun		China
34	Numerical Analysis of the Transient Response of Space Capsule Thermal Protection System for Re-entry Aerodynamic Heating	confirmed	Mr. khadar voli	Indian Space Research Organization (ISRO)	India
35	Simulation Method for Unilateralism Coupling of Diffusive and Deformation		Mr. YAO Dong	The 41st Institute of the Fourth Academy, China Aerospace Science and Technology Corporation (CASC)	China
36	Modelling and Dynamics of the Deployment of Mesh Antennas	confirmed	Dr. Zhihua Zhao	Tsinghua University	China
37	Robust Shape Design of Tension Truss Antennas on Variation of Tension Tie Forces	confirmed	Dr. Zhihua Zhao	Tsinghua University	China
38	Nonlinear elastic parameter identification of knitted wire mesh structure	confirmed	Prof. Tuanjie Li	Xidian University	China
39	Sprig driven expandable reflector for deployable antennas		Mr. Cristian Ambrosini		Italy
40	the design of a lightweight robotic arm link using functionally graded materials: a case study	confirmed	Mr. Thomas McMaster	University of Strathclyde, Glasgow	United Kingdom
41	probabilistic performances assessment for phase-change materials aided single-phase mechanically pumped fluid loops	confirmed	Dr. Jiaokun Cao	Key Laboratory of Space Utilization, Technology and Engineering Center for Space Utilization, Chinese Academy of Sciences	China
42	Waverider design with longitudinal stable self-trim characteristics	confirmed	Prof. Bingyan Chen	China Academy of Aerospace Aerodynamics (CAAA)	China
43	hypersonic simulation of mars entry atmosphere based on gun tunnel	confirmed	Mr. Feng Ji	China Academy of Aerospace Aerodynamics (CAAA)	China

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