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  • 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

    2018-10-04

    Time

    14:45

    Room

    ÖVB 2

    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

    Automated Thermal Model Correlation Tool for Space Applications

    12

    confirmed

    Mr. Alexander Milke

    ArianeGroup

    Germany

    2

    14:57

    Optimum Design and Thermal Analysis of Composite Insulation Structure Used in Cryogenic Storage Tanks on-orbit

    12

    withdrawn

    Mr. shaohua zhang

    China Academy of Launch Vehicle Technology(CALT)

    China

    3

    15:09

    Micro-pumped cooling loop to standardize micro-sat thermal control

    12

    confirmed

    Mr. Johannes van Es

    National Aerospace Laboratory (NLR)

    The Netherlands

    4

    15:21

    A backup system of a satellite orientation based on inverse problems technique

    12

    confirmed

    Prof. Aleksey V. Nenarokomov

    Moscow Aviation Institute

    Russian Federation

    5

    15:33

    Evaluation of thermal analysis of orbital environment of microsatellite ALE-1

    12

    confirmed

    Ms. Mina Konaka

    Tohoku University

    Japan

    6

    15:45

    The way of defining a powerful method for supersonic and hypersonic winged spacecraft aerodynamics prediction

    12

    confirmed

    Mrs. Olena Koliada

    Yuzhnoye State Design Office

    Ukraine

    7

    15:57

    Thermal Loads Simulators and Setup Strategies of Thermal Tests for Small Satellites

    12

    confirmed

    Mr. Roy Stevenson Soler Chisabas

    Brazilian National Institute for Space Research - INPE

    Brazil

    8

    16:09

    Unsteady Coupled Heat Transfer Simulations of Hypersonic Gap Flows

    12

    withdrawn

    Dr. Qiang Wang

    China

    9

    16:21

    Using the “Comparative Test Method” to Determine the Heat Statuses for the Heat Shields of Spacecraft

    12

    confirmed

    Prof. Oleg Alifanov

    Moscow Aviation Institute

    Russian Federation

    10

    16:33

    Experimental and Numerical Study on the PCM Thermal Control Device for Spacecraft Electronics

    12

    confirmed

    Prof. Taig Young Kim

    Korea Polytechnic University

    Korea, Republic of

    11

    16:45

    Thermal Control of High Power Applications on CubeSats

    12

    confirmed

    Ms. Katja Janzer

    Technische Universität München

    Germany

    12

    16:57

    The Influence of Shock Wave on Ablation Thermal Environment of Re-entry Vehicle Protuberance

    12

    confirmed

    Mr. dongbin ou

    China Academy of Aerospace Aerodynamics (CAAA)

    China