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  • session 1

    Title

    Space Structures I - Development and Verification (Space Vehicles and Components)

    type

    oral

    Description

    The topics addressed in this session cover the aspects of the development and verification of space vehicle structures (e.g. pressurized propellant tanks, non-pressurized structures of space vehicles, control surfaces) and their components (e.g. fluidic equipment and propulsive lines). The aspects of development, verification, and qualification concern: • Thermo-Mechanical loads and environment • New structural concepts (e.g. multi-functional structures, design concepts for reusability) • Structure design and verification (stiffness, strength, static and dynamic stability, damage tolerance, reusability) • Structure optimization • Materials • Static and dynamic ground testing • Exploitation of flight measurements and in-orbit testing • Lessons learned related to space vehicle structures and components development, verification and qualification

    Date

    2023-10-02

    Time

    15:15

    Room

    BCC A1

    IPC members
    • Co-Chair: Prof. Paolo Gasbarri, University of Rome “La Sapienza”, Italy;

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

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    15:15

    Synthesis of dicarboxylate derivatives with antimicrobial properties

    12

    confirmed

    Ms. Zahra Fataliyeva

    Azerbaijan State Oil and Industry University (ASOIU)

    Azerbaijan

    2

    15:27

    Windows for Space Applications

    12

    withdrawn

    Dr. Annamaria Piras

    Thales Alenia Space Italia

    Italy

    3

    15:39

    Morphology of Polyhedral Space Habitat Modules - Identifying the Ideal Form Using Multi-Criteria Analysis

    12

    confirmed

    Mr. Elliott Ruzicka

    United States

    4

    15:51

    Innovative solutions for space habitable structures

    12

    withdrawn

    Mr. Simone Ambrosino

    Politecnico di Torino

    Italy

    5

    16:03

    Passive thermal expansion compensation mechanism design using FEM for off-axis optical payload in Low Earth Orbit small satellite

    12

    confirmed

    Mr. Pearachad Chartsiriwattana

    National Astronomical Research Institute of Thailand (NARIT)

    Thailand

    6

    16:15

    Effect of geometric parameters of constituent members on the structural behaviour of the lattice truss beam for space applications

    12

    confirmed

    Dr. Litesh Sulbhewar

    University of Glasgow

    United Kingdom

    7

    16:27

    A pneumatic separation system for rocket separation

    12

    confirmed

    Mrs. aizhen ming

    CAS Space

    China

    7

    16:27

    \textbf{Space Structures: Development and Verification}

    12

    withdrawn

    Mr. Shryas Bhurat

    R V College of Engineering, Bengaluru

    India

    8

    16:51

    INVESTIGATION OF INTEGRATION OF ANNULAR FIN CONFIGURATION AND GEOMETRY FOR IMPROVED THERMAL MANAGEMENT OF ROCKET NOZZLES: DESIGN, ANALYSIS, AND OPTIMIZATION

    12

    confirmed

    Mr. Sriram Kumar

    Sri Sairam Engineering College

    India

    10

    17:03

    Design optimization of cubic in shape pressurant tank for cubesat's propulsion system

    12

    confirmed

    Dr. Georgy Shcheglov

    Bauman Moscow State Technical University

    Russian Federation