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  • session 1

    Title

    Space Structures I Design, Development and Verification (Launch Vehicles and Space Vehicles, including their Mechanical/Thermal/ Fluidic Systems)

    type

    oral

    Description

    The topics addressed in this session cover the aspects of the design, development and verification of space launch system structures (e.g. pressurized propellant tanks, non-pressurized structures of space vehicles, control surfaces) and their components (e.g. fluidic equipment and propulsive lines, thermal control systems). The aspects of design, 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) • design, verification and qualification of fluidic and thermal control systems • 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

    2025-09-29

    Time

    15:30

    Room

    Room C3.4

    IPC members
    • Co-Chair: Mr. Alwin Eisenmann, IABG Industrieanlagen - Betriebsgesellschaft mbH, Germany;

    • Co-Chair: Dr. Jochen Albus, ArianeGroup, Germany;

    • Rapporteur: Dr. Zijun Hu, China Academy of Launch Vehicle Technology (CALT), China;

    • Rapporteur: Ms. Coraline Dalibot, Rutherford Appleton Laboratory, United Kingdom;

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    15:30

    Discovering the Applications of the Neglected Classification Surrogate for Rocket Design Optimization

    10

    Mr. Said Mouhaiche

    The University of Sydney

    Australia

    2

    15:40

    Internally Fastened Manhole Cover for Lightweight Composite Propellant Tanks

    10

    Dr. Youngha Yoon

    Korea Aerospace Research Institute (KARI)

    Korea, Republic of

    3

    15:50

    Study of Axial Compression Bearing Capacity of Stainless Steel Tanks in Reusable Launch Vehicle

    10

    Mrs. Pei Li

    LandSpace Technology Corporation Ltd.

    China

    4

    16:00

    study on a novel spacecraft thermal control system based on phase change heat storage

    10

    Dr. Dong La

    Shanghai Institute of Satellite Engineering

    China

    5

    16:10

    Thermal and Structural Analysis of Space-Based Solar Power Satellites (SBSP) in Geostationary Orbit

    10

    Mr. Fawzan Mohamed Kareem Navaz

    Amity University, Dubai

    United Arab Emirates

    6

    16:20

    Analytical Framework for Assessment of Fatigue Life in Additive Manufacturing based Superalloys for Propulsion Applications and its Implementation in a Model-based Environment

    10

    Ms. Danielle McDowell

    University of Alabama in Huntsville

    United States

    7

    16:30

    Design, Analysis and Comparison of Biomimetic Hierarchical Honeycomb Sandwich Composites for Aerospace Applications

    10

    Mr. DINENDRA ARCOT VISWANATH

    Politecnico di Milano

    Italy

    8

    16:40

    Development of a Thermal Vacuum Optical System for Testing Earth Observation Imagers

    10

    Mr. Nicolaas Vlok van Jaarsveld

    Simera Sense

    South Africa

    9

    16:50

    Composite Materials and Manufacturing Methods for Hydrogen Storage for Space Systems

    10

    Ms. zuleyha savci

    Ankara Yıldırım Beyazıt University

    Türkiye

    10

    17:00

    Multifuctional Energy Dense Structural Composites for Advanced Satellite Systems

    10

    Mr. Shryas Bhurat

    U.C. Berkeley

    United States

    11

    17:10

    structural design and simulation analysis of alter: a high-mobility rover for multi-terrain locomotion and mission support

    10

    Ms. Farha Hassan Priti

    BRAC University

    Bangladesh

    12

    17:20

    Numerical Modeling and Analysis of the Combined Effects of Thermal, Dynamic, and Shock Loadings on the Reliability and Lifetime Prediction of Space Electronic Boards

    10

    Prof. Seyed Mohammad Navid Ghoreishi

    Satellite Research Institute, Iranian Space Research Center

    Iran

    13*

    17:30

    Advancing Optical Payload Qualification: Planet’s Optical Test Lab and the Development of State-of-the-Art Ground Support Equipment

    10

    Mr. Farbod Akhavan Niaki

    Planet

    United States

    14*

    17:30

    Damage Identification Model of Re-entry Capsule Based on Field Information Inversion

    10

    Mr. Jia-Xin Hu

    Northwestern Polytechnical University

    China