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  • IAC-17
  • C2
  • 7
  • session 7

    Title

    Space Vehicles – Mechanical/Thermal/Fluidic Systems

    type

    oral

    Description

    The topics to be addressed include novel technical concepts for mechanical/thermal/fluidic systems and subsystems of launchers, manned and unmanned spacecraft, re-entry vehicles and small satellites. Advanced subsystems and design of future exploration missions will be covered, considering issues arising from material selection, cost efficiency and reliability, and advancements in space vehicle development with respect to engineering analysis, manufacturing, and test verification.

    Date

    2017-09-28

    Time

    14:45

    Room

    Panorama Room 2

    IPC members
    • Co-Chair: Dr. Brij Agrawal, Naval Postgraduate School, United States;

    • Co-Chair: Prof.Dr. Oleg Alifanov, MAI, Russian Federation;

    • Rapporteur: Prof. Guoliang Mao, Beijing Institute of Aerodynamics, China;

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    A novel design approach for space components: application to a multifunctional panel

    12

    confirmed

    Mr. Andrea Emanuele Maria Casini

    Politecnico di Torino

    Italy

    2

    thermal optical analysis of LAPAN's IR camera

    12

    no-show

    Mr. Bustanul Arifin

    Indonesian National Institute of Aeronautics and Space (LAPAN)

    Indonesia

    3

    The Building Block of Small Space Mechanisms and Robots - A Micro Actuator with High Torque/Weight Ratio

    12

    confirmed

    Dr. Rui Li

    Beijing Institute of Control Engineering, China Academy of Space Technology

    China

    4

    Lightweight Means of Actuation for Use in Space-Based Robotics Applications

    12

    withdrawn

    Mr. Scott Brady

    University of Strathclyde, Glasgow

    United Kingdom

    5

    Experimental study of Heat Switch Radiator using Shape Memory Alloy for High Insulation System

    12

    confirmed

    Mr. Shunsaku Eguchi

    Tokyo University of Science

    Japan

    6

    A STUDY OF ELECTROMAGNETIC ENVIRONMENTAL EFFECTS ON SPACE LAUNCH SYSTEMS BY MEANS OF REVERBERATION CHAMBER

    12

    confirmed

    Dr. Marta Albano

    Agenzia Spaziale Italiana (ASI)

    Italy

    7

    Coupled Thermodynamic and Structural Optimization of a Cryogenic Upper Stage into GEO

    12

    confirmed

    Mr. Marco Vietze

    Universität der Bundeswehr München

    Germany

    8

    Enhancement of Thermal Control Performance by Using Liquid Metal Radiator

    12

    confirmed

    Mr. Tae-Yong Park

    Chosun University

    Korea, Republic of

    9

    A trade-off study on the mechanical support structure of the MASCOT-2 small body lander package

    12

    confirmed

    Mr. Michael Lange

    DLR (German Aerospace Center)

    Germany

    10

    Qualification of an Infrared Array Based on NiCr Strips for CBERS 4A Satellite’s Space Simulation Test

    12

    withdrawn

    Mr. George Fernandes

    National Institute for Space Research - INPE

    Brazil

    11

    design and on-board validation of pumped two-phase fluid loop for high heat flux removal

    12

    confirmed

    Dr. xingang yu

    China

    12

    The design of a satellite with a structure of Rubik's cube

    12

    withdrawn

    Ms. Qi Chen

    CAST

    China

    13

    compression failure mechanisms in sandwich panels with corrugated channel cores

    12

    confirmed

    Mr. Zhenyu Zhao

    Xi'an Jiaotong University

    China

    14

    Aeroheating Analysis of RCS Jet Interaction Effects on the RLV

    12

    confirmed

    Dr. Xiaoyan Li

    CALT,CASC

    China

    15

    European REACH legislation: Impact on European launchers and current activities on new sustainable technologies

    confirmed

    Ms. Marie-Christine Contino

    European Space Agency (ESA)

    France