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  • IAC-15
  • C2
  • IP
  • session IP

    Title

    Interactive Presentations

    type

    interactive

    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

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    Dynamics Analysis of Flexible Cone Undergoing Space Docking

    Dr. wei han

    National University of Defense Technology

    China

    Ka Band Metal Wire Mesh Development for Deployable Reflector

    withdrawn

    Dr. XiaoFei Ma

    Xi’an Institute of Space Radio Technology

    China

    A new multi-layer and graded-density flexible ablator

    Ms. Luo Lijuan

    China

    research on the frequency characterization method of structural design

    confirmed

    Dr. Linan SHI

    Science and Technology on Space Physics Laboratory

    China

    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

    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

    Transfer Path Analysis of Dynamic Loading for the Second stage Liquid Rocket Engine

    Dr. Binchao Li

    Xi'an Aerospace Propulsion Institute

    China

    The influence factor of the dispersibility of carbon nano tube in epoxy resin

    Mr. zhou fang

    China Academy of Launch Vehicle Technology(CALT)

    China

    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    withdrawn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

    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    withdrawn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

    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

    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

    a new approach based on metallographic analysis and micro Hardness test on evaluating the temperature of reusable ramjet engine

    confirmed

    Mr. ren jiawan

    China

    structural design and topology optimization of a university micro-satellite

    Ms. Jing Guo

    School of Astronautics, Beihang University

    China

    an immersed boundary method for compressible flow simulation

    confirmed

    Mr. YueLong He

    China Academy of Aerospace Aerodynamics (CAAA)

    China

    Study on Satellite segment vibration test technology

    withdrawn

    Mr. Hao Jiang

    China

    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

    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

    The establishment of dynamic model for the single-phase fluid loop system

    Mr. Fanjian Zeng

    China

    Experimental Investigation on the Decomposition Rate of Phenolic Resin Thermal Protection Material

    confirmed

    Mr. Jian-qiang Tu

    China Academy of Aerospace Aerodynamics (CAAA)

    China

    CVD methods for graphene generation on stainless steels for corrosion resistance

    withdrawn

    Mr. Michael Eisfelder

    Monash University

    Australia

    Aerodynamic force and heat fast prediction for high speed vehicles based on effective numerical and engineering methods

    confirmed

    Mr. rong wang

    China

    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

    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

    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

    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

    REACTION CONTROL OF FLEXIBLE JOINT SPACE MANIPULATORS

    Dr. Silvio Cocuzza

    CISAS – “G. Colombo” Center of Studies and Activities for Space, University of Padova

    Italy

    Time-variant Reliability Analysis of Cabin's Door Considering Component Damage

    confirmed

    Dr. lin ye

    China

    Verification with quasi-static tests of composite structures for launchers, satellite and re-entry vehicles

    confirmed

    Dr. Davide Santachiara

    DTM srl

    Italy

    Design and verification of high pressure high purity gas delivery systems for International Space Station

    confirmed

    Dr. Davide Santachiara

    DTM srl

    Italy

    Investigation of Cabin Pressure Prediction for Intake and Exhaust System on Re-entry Vehicles

    Mrs. Huiling Zhan

    China Academy of Aerospace Aerodynamics (CAAA)

    China

    A rapid method to calculate the viscous force based on local inviscid flow field parameters

    withdrawn

    Mr. Gong Anlong

    China

    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

    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

    epoxy based shape memory polymers for space applications

    confirmed

    Ms. Debby Margoy

    SOREQ NRC

    Israel

    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

    cnt-polyimide nanocomposites for space applications

    confirmed

    Mrs. Nurit Atar

    SOREQ NRC

    Israel

    Dynamic characteristic analysis of a moment control unit with vibration isolation capability and its application

    Dr. Yao Zhang

    Beijing Institute of technology(BIT)

    China

    Application of RANS/LES in Computing Hypersonic Turbulent Base Heating

    confirmed

    Mr. Xingliang Sun

    Beihang University (BUAA)

    China

    The Design and Testing of Deployment Mechanisms and Structure of Twin Nano-Satellite, STUDSAT-2.

    confirmed

    Mr. Nikhilesh K V

    NMAMIT NITTE

    India

    Reduction of processing time and human factor effects during the strength assessment of the spacecraft structure

    confirmed

    Mr. Nikolay Asmolovskiy

    Space Structures GmbH

    Germany

    research on repeatable locking mechanism for space solar array

    withdrawn

    Mr. Lei Jia

    China Academy of Launch Vehicle Technology(CALT)

    China

    Fold-Deployment Concept and Prototype Design for Air-Inflatable Solar Sail

    confirmed

    Ms. ZhengAi Cheng

    Qian Xuesen Laboratory of Space Technology

    China

    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

    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

    Mechanism and kinetic characterization of the electron irradiation induced degradation of DGEBA/DICY

    Dr. gang liu

    China Academy of Space Technology (CAST)

    China

    Development and Study of Micro-Vibration Simulation Analysis System for Small Satellites

    confirmed

    Dr. Zhi Yang

    DFH Satellite Co. Ltd.

    China

    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

    shape optimization of inside-hole in triangular ribbed plate

    confirmed

    Ms. Yiqian Zhou

    China

    A Boundary Element Method for Transient Nonlinear Radiative-Conductive Coupled Heat Transfer Problems

    confirmed

    Dr. wang jing

    CASC

    China

    on the development of arc tunnel test technology for control surface seal evaluations

    confirmed

    Mr. zhang qian

    China Academy of Aerospace Aerodynamics (CAAA)

    China

    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