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  • session IP

    Title

    Interactive Presentations

    Description

    Authors with an abstract accepted for an interactive presentation will be asked to prepare slides and display them for the duration of the congress on plasma screens. Authors will be assigned to interactive sessions in which they must be near the plasma screens to engage in interactive discussions with other congress attendees.

    Date

    2016-09-28

    Time

    13:15

    Room

    Jalisco Hall C - Exhibition Hall

    IPC members
    • Coordinator: Dr. Constantinos P. Stavrinidis, IABG Industrieanlagen - Betriebsgesellschaft mbH, Germany;

    • Coordinator: Prof. Pavel M. Trivailo, RMIT University, Australia, Australia;

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    time delay estimation control of flexible-joint dual-arm space robot

    confirmed

    Dr. Jie Liang

    China

    2

    Magnetic flame spread

    confirmed

    Mr. Pratik Tiwari

    SRM University Chennai

    India

    3

    parametric study on the design of the thermal control equipment using the phase change material

    confirmed

    Prof. Taig Young Kim

    Korea Polytechnic University

    Korea, Republic of

    4

    Design Method for Drilling and Sampling Device with Axial Hammering Pattern

    confirmed

    Dr. Yuanxun Zhang

    Center of Space Exploration, Ministry of Education (COSE)

    China

    5

    Assessment of structural integrity of HPS3 flex seal sub assembly to convergent sub assembly under reduced pre load condition

    confirmed

    Mr. Arun Krishnan

    Indian Space Research Organization (ISRO)

    India

    6

    Collision Analysis for Free-flying Space Manipulator with Flexible Arms Impacted by a Satellite Adaptive Neural Network Control and Vibration Suppression for Combined System

    withdrawn

    Dr. Jing Cheng

    Fuzhou University

    China

    7

    The experimental study of surface catalytic effect on the stagnation heat-transfer rates in high-enthalpy shock tube

    confirmed

    Mr. Zhang Hongjun

    Beijing Aerospace Technology Institute

    China

    8

    Spacecraft Ejection Mechanism Using Sodium Azide

    Mr. Subham Gupta

    SRM University, kattankulathur, chennai, INDIA

    India

    9

    Investigation on heat transfer of submerged water jet impingement on micro-channel heat sink

    confirmed

    Ms. Yao Pan

    China Academy of Launch Vehicle Technology R&D Center

    China

    10

    Space Simulation Chambers State-of-the-Art

    confirmed

    Mr. Roy Stevenson Soler Chisabas

    Brazilian National Institute for Space Research - INPE

    Brazil

    11

    A Radiation Hardened Multicore DSP Processor Designed for Space Missions

    confirmed

    Mr. Hui Cao

    Xi'an Microelectronics Technology Institute, China Aerospace Science and Technology Corporation (CASC)

    China

    12

    unsteady numerical simulation and attitude control on separation trajectories of missile ejected from aircraft

    confirmed

    Mr. Wei Yang

    Beijing Electro-Mechanical Engineering Institute, China Aerospace Science & Industry Corporation (CASIC)

    China

    13

    Design criticalities and structural integrity analysis of the spin-stabilization solid rocket motor charged with high energy grain

    confirmed

    Mr. Shitij Arora

    Vikram Sarabhai Space Centre (VSSC)

    India

    14

    Reaction Control of a Space Manipulator with Compliant Joints

    withdrawn

    Dr. Silvio Cocuzza

    Space Mechatronic Systems Technology Laboratory, University of Strathclyde

    United Kingdom

    15

    Investigation of an effective approach for aerodynamics computation of Mars entry vehicles

    Mrs. Huiling Zhan

    China Academy of Aerospace Aerodynamics (CAAA)

    China

    16

    Method for CubeSat Thermal-Vacuum testing specifications

    confirmed

    Mr. Roy Stevenson Soler Chisabas

    Brazilian National Institute for Space Research - INPE

    Brazil

    17

    first stage aerodynamic optimization of the launch vehicle in landing area control technology

    confirmed

    Mr. Linfei Du

    China