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    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, Sapienza University of Rome, Italy;

    • Co-Chair: Dr. Andreas Rittweger, DLR (German Aerospace Center), Germany;

    papers

    Order

    Presentation status

    Mode

    Paper title

    Speaker

    Affiliation

    Country

    1

    withdrawn

    A brief discussion about force control of robot manipulators

    Mr. Vinicius Piro Barragam

    ITA-DCTA

    Brazil

    2

    withdrawn

    Synthesis and Characterization of Pr(3-x)Te(4) and Nd(3-x)Te(4) for High Temperature Thermoelectric Applications

    Mr. Dean Cheikh

    University of California, Los Angeles (UCLA)

    United States

    3

    withdrawn

    Analysis of type II and type III solar radio bursts using the e - CALLISTO system

    Mr. Jude Wijesekera

    Sri Lanka

    4

    withdrawn

    Additive Manufactured Aerospike Reaction Control System

    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

    confirmed

    Water-Cooled Adjustable Material Probe Design for the Evaluation of Transient Heat Fluxes of High Temperature Materials

    Mr. Nicholas Harmansa

    IRS, University of Stuttgart

    Germany

    7

    confirmed

    Research on buffer mechanism and impact dynamics of pre-folded metal honeycomb structure

    Dr. Na Yao

    Qian Xuesen Laboratory of Space Technology, China Academy of Space Technology (CAST)

    China

    8

    withdrawn

    a new approach for the environmental adaptability design, analysis and verification of a large spacecraft

    Dr. Xinyu Zhang

    Beijing Institute of Aerospace Systems Engineering, China Aerospace Science and Technology Corporation (CASC)

    China

    9

    withdrawn

    flight results of structure subsystem for enhanced epsilon launch vehicle

    Mr. Hiroshi Ikaida

    Japan Aerospace Exploration Agency (JAXA)

    Japan

    10

    confirmed

    Ground and stratospheric flight tests on curing of composite materials in free space environment

    Prof. Alexey Kondyurin

    The University of Sydney

    Australia

    11

    confirmed

    Investigation of Co-Sn-Te Phase Space for Advancement of Skutterudite Materials for Radioisotope Thermoelectric Generators

    Ms. Caitlin Crawford

    Colorado School of Mines, NASA Harriett G. Jenkins Fellow

    United States

    12

    confirmed

    Energetic Composite Solid Propellants for advanced space systems

    Mr. vinayak malhotra

    SRM University Chennai

    India

    13

    withdrawn

    Honeycomb Propellant Tank Design used for SRMSAT - 2

    Mr. Subham Gupta

    SRM University, kattankulathur, chennai, INDIA

    India

    14

    confirmed

    Dimensional stability investigation of low CTE materials at temperatures from 140 K to 250 K using a heterodyne interferometer

    Ms. Ines Hamann

    DLR (German Aerospace Center)

    Germany

    15

    confirmed

    Characterization of Direct Metal Laser Sintered Impinging Injectors: Like-Doublet, Unlike Triplet, Like Quadlet, Unlike Pentad

    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

    confirmed

    Analysis and Verification of Bearing Capacity of Stiffened Panel of Carbon Fiber Reinforced Polymer Composites

    Mr. CUI Shenshan

    China Academy of Launch Vehicle Technology (CALT)

    China

    18

    confirmed

    Problems of Modelling in dynamics of stabilization and orientation systems

    Prof. Lyudmila Kuzmina

    Kazan National Research Technical University

    Russian Federation

    19

    withdrawn

    optimization of cylindrical composite material grid structure

    Mr. Ilan Weissberg

    Israel Aerospace Industries Ltd.

    Israel

    20

    withdrawn

    Characterization of Porosity via MicroCT for Selectively Laser Melted Titanium-64 and Inconel 718

    Mr. Alexander Finch

    Purdue University

    United States

    21

    withdrawn

    The study on materials thermal properties and optimal design for solar probe thermal protection

    Prof. Oleg Alifanov

    Moscow Aviation Institute

    Russian Federation

    22

    confirmed

    A Multidisciplinary Software Chain for Integrated Structural, Thermal and Optical Performance Analysis of Space Instruments

    Dr. Stefan Bedrich

    OHB System AG - Munich

    Germany

    23

    confirmed

    Model Updating of Thermo-Elastic Plates of Spacecrafts in the Hot and Cold Space Environments

    Dr. Kaipeng Sun

    Shanghai Institute of Satellite Engineering

    China

    24

    confirmed

    Testing and modeling for the creep and recovery behavior of Kevlar cables

    Prof. Tuanjie Li

    Xidian University

    China

    25

    confirmed

    Structural Dynamic Modification for Shock Response Spectra Test of a Fixture Based on Sensitivity Analysis of Anti-resonance Frequency

    Dr. DENG Changhua

    Xi'an Aerospace Propulsion Institute

    China

    26

    withdrawn

    Revealer1601-RH : A radiation hardened NoC-based Multicore Digital Signal Processor

    Dr. Hui Cao

    Xi'an Microelectronics Technology Institute, China Academy of Space Electronics Technology (CASET), China Aerospace Science and Technology Corporation (CASC)

    China

    27

    confirmed

    Paraffin-graphene/metal foam composite for thermal management in electronics

    Dr. Adriana Balan

    University of Bucharest (UB)

    Romania

    28

    confirmed

    Experimental Studies on Supersonic Aerothermal Fluid-Structure Interaction

    Mr. Dennis Daub

    DLR (German Aerospace Center)

    Germany

    29

    confirmed

    application of composite sandwich structure with lattice cores in aircraft lightening design

    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

    confirmed

    A Fully Configurable Mass Dummy Design for Changing Spacecraft Structures

    Mr. Mehdi Sabzalian

    Space Flight Laboratory, University of Toronto

    Canada

    32

    confirmed

    The prospect of additive manufacturing in primary structure of launch vehicle

    Dr. Ji Bin

    Aerospace System Engineering Shanghai, China

    China

    33

    confirmed

    experiments on residual compressive strength after fatigue of cabon fiber fabric composites of spacecraft in hydrothermal environment

    Dr. xuan sun

    China

    34

    confirmed

    Numerical Analysis of the Transient Response of Space Capsule Thermal Protection System for Re-entry Aerodynamic Heating

    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

    confirmed

    Modelling and Dynamics of the Deployment of Mesh Antennas

    Dr. Zhihua Zhao

    Tsinghua University

    China

    37

    confirmed

    Robust Shape Design of Tension Truss Antennas on Variation of Tension Tie Forces

    Dr. Zhihua Zhao

    Tsinghua University

    China

    38

    confirmed

    Nonlinear elastic parameter identification of knitted wire mesh structure

    Prof. Tuanjie Li

    Xidian University

    China

    39

    Sprig driven expandable reflector for deployable antennas

    Mr. Cristian Ambrosini

    Italy

    40

    confirmed

    the design of a lightweight robotic arm link using functionally graded materials: a case study

    Mr. Thomas McMaster

    University of Strathclyde, Glasgow

    United Kingdom

    41

    confirmed

    probabilistic performances assessment for phase-change materials aided single-phase mechanically pumped fluid loops

    Dr. Jiaokun Cao

    Key Laboratory of Space Utilization, Technology and Engineering Center for Space Utilization, Chinese Academy of Sciences

    China

    42

    confirmed

    Waverider design with longitudinal stable self-trim characteristics

    Prof. Bingyan Chen

    China Academy of Aerospace Aerodynamics (CAAA)

    China

    43

    confirmed

    hypersonic simulation of mars entry atmosphere based on gun tunnel

    Mr. Feng Ji

    China Academy of Aerospace Aerodynamics (CAAA)

    China