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  • 7
  • session 7

    Title

    Space Vehicles – Mechanical/Thermal/Fluidic Systems

    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

    2015-10-15

    Time

    14:45

    Room

    Oranim 1 (ICC, lower level)

    IPC members
    • Co-Chair: Prof. Oleg Alifanov, Moscow Aviation Institute, Russian Federation;

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

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

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    14:45

    Performance Analysis of a Vapor Compression Heat Pump System for Solar Power Satellites

    12'

    confirmed

    Dr. Na Yao

    Qian Xuesen Laboratory of Space Technology

    China

    2

    14:57

    Further Developments in the 3Omega Thermal Conductivity and Diffusivity Measurement System

    12'

    confirmed

    Dr. Matthew Dalton

    Sonaca Space GmbH

    Germany

    3

    15:09

    DEVELOPMENT OF THERMAL CAPACITORS FOR TEMPERATURE REGULATION IN SPACECRAFT

    12'

    confirmed

    Dr. Matthew Dalton

    Sonaca Space GmbH

    Germany

    4

    15:21

    Experimental study of the start-up heat and mass transfer performances of porous plate water sublimator combined with fluid loop

    12'

    confirmed

    Dr. Yuying WANG

    Beijing Institute of Spacecraft System Engineering, China Academy of Space Technology

    China

    5

    15:33

    A study on mechanism and experiment of pump-assisted capillary phase change loop

    12'

    no-show

    Mr. Xiaoyu Zhang

    China Academy of Launch Vehicle Technology(CALT)

    China

    6

    15:45

    Inverse thermal analysis for reentry vehicles

    12'

    confirmed

    Prof. Sterian Danaila

    University POLITEHNICA of Bucharest - Research Center for Aeronautics and Space

    Romania

    7

    15:57

    A lightweight cargo carrier spacecraft thermal control system design technology

    12'

    confirmed

    Prof. chuanfeng wei

    Institute of Manned Space System Engineering,China Academy of Space Technology (CAST)

    China

    8

    16:09

    Cryogenic technics in russian scientific space missions

    12'

    no-show

    Mr. Anton Burdanov

    Central Research Institute for Machine Building (FGUP TSNIIMASH)

    Russian Federation

    9

    16:21

    a new concept of variable resistance radiator: stratospheric flight test & performance analysis

    12'

    confirmed

    Mr. Davide Paganini

    University of Padova

    Italy

    10

    16:33

    thermal loads simulation array in a typical satellite thermal control surface.

    12'

    confirmed

    Dr. Marcio Bueno dos Santos

    Instituto Nacional de Pesquisas Espaciais (INPE)

    Brazil

    11

    16:45

    Assessment of a low-cost multilayer insulation system for thermal control of nanosatellites

    12'

    confirmed

    Mr. Riccardo Di Roberto

    G.A.U.S.S. Srl

    Italy

    12

    16:57

    Solar Orbiter Heat Shield Thermal performance demonstrated on STM

    12'

    no-show

    Dr. Annamaria Piras

    Thales Alenia Space Italia

    Italy