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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

    2009-10-16

    Time

    10:00

    Room

    Technical Session #5

    IPC members
    • Chairman: Prof. Mario Marchetti, Sapienza University of Rome, Italy;

    • Chairman: 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

    AMS02 Tracker Thermal Control Cooling system overview and spin-off for future spacecraft cooling system developments

    20'

    Mr. Johannes van Es

    Netherlands Aerospace Centre (NLR)

    The Netherlands

    2

    Technical Appearance Selection of Action Module on the Asteroid “Apophis” and Integration of this Module with Launch Vehicle

    20'

    Dr. Stanislav Konyukhov

    Yuzhnoye State Design Office

    Ukraine

    3

    The interactive mechanism research of heat environment and thermal protection material

    20'

    Dr. Bangcheng Ai

    China Aerospace Science and Industry Corporation

    China

    4

    BASE FLOW FIELD, PRESSURE AND DRAG DURING ATMOSPHERIC REENTRY OF A RETRIEVABLE ORBITAL VEHICLE

    20'

    Mr. Col. Jose Duarte

    Instituto de Aeronáutica e Espaço (IAE)

    Brazil

    5

    High-Porous Aerospace Materials: Identification and Prediction of Physical Properties

    20'

    Prof. Aleksey V. Nenarokomov

    Moscow Aviation Institute

    Russian Federation

    7

    optimization of a space based heat pipe radiator

    20'

    Mr. Kien Hung

    Beijing University of Aeronautics and Astronautics (BUAA)

    China

    8

    Thermal Balance Testing the TM of the China-Brazil Remote Sensing Satellite

    20'

    Dr. Jose Sergio Almeida

    Instituto Nacional de Pesquisas Espaciais (INPE)

    Brazil

    9

    Thermal Design of Earth Observation Satellite (KOMPSAT-3 and 5) using Ground Test Data

    20'

    Dr. Bum-Seok Hyun

    Korea Aerospace Research Institute (KARI)

    Korea, Republic of

    10

    A ground-based test method for spaceship active thermal control system

    20'

    Dr. xingang yu

    China

    11

    Future directions of multi-use reentry thermal protection systems for winged vehicles

    20'

    Mr. Slawomir Zdybski

    International Space University (ISU)

    France

    12

    FINITE ELEMENT ANALYSIS FOR SANDWICH BEAMS

    20'

    Mr. Shanti Swaroop Kandala

    Young India Fellowship Programme

    India