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  • IAC-22
  • 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.

    Date

    2022-09-21

    Time

    15:00

    Room

    W06

    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;

    • Rapporteur: Dr. Federica Angeletti, University of Rome “La Sapienza”, Italy;

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    15:00

    Multi-engines cryogenic stage low-cost structures and fluid components for small satellites launch services

    12

    confirmed

    Mr. Maxime HEGO

    France

    2

    15:12

    Experimental Validation of a Solid State Magnetocaloric Cooler in a Space Environment

    12

    confirmed

    Mr. Markus Huwald

    Technische Universität Braunschweig, Institute of Space Systems

    Germany

    3

    15:24

    Analysis of effective thermal control designs for small satellites

    12

    confirmed

    Ms. Anvesha Yadav

    R.V.College of Engineering

    India

    4

    15:36

    POGO Characteristics and Experimental Analysis of the First Chinese Liquid Oxygen-Methane Launcher “ZQ-2”

    12

    confirmed

    Dr. wenbin cao

    LandSpace Technology Corporation Ltd.

    China

    5

    15:48

    thermal balance and thermal vacuum test of the cbers-4a satellite performed at inpe, brazil.

    12

    confirmed

    Dr. Geilson Loureiro

    National Institute for Space Research - INPE

    Brazil

    6

    16:00

    EFFECTIVENESS OF A BELLY FLAP IN MARTIAN ATMOSPHERE

    12

    confirmed

    Ms. Spoorthi M.S.

    University of Petroleum and Energy Studies

    India

    7

    16:12

    Temperature distribution along a composite and metallic shell in cryogenic environment

    12

    confirmed

    Mr. Prashumn Prashumn

    Indian Space Research Organization (ISRO), Liquid Propulsion Systems Centre (LPSC)

    India

    8

    16:24

    Influence of hydrogen and oxygen self-pressurizing temperature on heat transfer of propellant tank

    12

    confirmed

    Dr. Liqiang Ai

    China Academy of Launch Vehicle Technology (CALT)

    China

    9

    16:36

    Designing the first three-section arm on a CubeSat

    12

    confirmed

    Ms. Juliette Lacasse

    Université de Sherbrooke

    Canada

    10

    16:48

    Structural design of a CubeSat type nanosatellite for academic purposes.

    12

    confirmed

    Mr. Edwin Cruz Martínez

    Mexico

    11

    17:00

    Additively Manufactured High-Power-Density Cold Plates

    12

    confirmed

    Ms. Jana Catuche

    United States

    12

    17:12

    The fabrication and application of water sublimator heat dissipation system in Chang'e 5 lunar probe

    12

    Dr. Yuying WANG

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

    China