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  • IAC-20
  • C2
  • 7
  • session 7

    Title

    Space Vehicles – Mechanical/Robotic/Thermal/Fluidic Systems

    type

    oral

    Description

    The topics to be addressed include novel technical concepts for mechanical/robotic/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. It is also planned to discuss the issues of experimental and computational simulation of functioning and full-scale tests of space vehicles and their systems/subsystems. Attention will be paid to the problem of verification and validation of mathematical models for the design and experimental development of these objects at various phases of their life cycle.

    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

    5

    DIAGNOSTICS OF DEFECTS OF THERMAL PROTECTIONS INFLATABLE RE-ENTRY VEHICLES

    confirmed

    Dr. Alena V. Morzhukhina

    Moscow Aviation Institute (National Research University, MAI)

    Russian Federation

    9

    Attitude control system of a microsatellite based on the inverse problems technique and the Kalman filter

    10

    confirmed

    Mr. Evgeny Chebakov

    Moscow Aviation Institute (National Research Institute, MAI)

    Russian Federation

    10

    Reliability-based multi-objective design optimization of the satellite thermal control system using swarm-based optimization algorithms

    10

    confirmed

    Mr. Elyas Fadakar

    Beihang University (BUAA)

    China

    12

    Development of a thermal design model for a small spacecraft with integrated heat pipes

    10

    confirmed

    Mr. Nikolay Mullin

    Skolkovo Institute of Science and Technology

    Russian Federation

    13

    MONITORING AND ANALYSIS OF THE STRESSED-DEFORMED CONDITION OF THE SHELLS, IN THE PROCESS OF THEIR MANUFACTURE DURING 3D PRINTING AND WELDING WORKS

    10

    confirmed

    Mr. Valerii Satokin

    Ukraine

    15

    Cooling Channel at the Leading Edge of Supersonic Vehicle design based on Working fluid convection

    10

    confirmed

    Ms. Mochen Chang

    Northwestern Polytechnical University

    China

    16

    SharjahSat-1 Thermal Analysis for Orbit-Launch Selection

    10

    confirmed

    Mr. Ibrahim Alsabt

    Sharjah Academy for Astronomy, Space Sciences and Technology (SAASST)

    United Arab Emirates