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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)

    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

    2024-10-14

    Time

    15:15

    Room

    Orange Hall 1

    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

    15:15

    enhancing crashworthiness of legged-type lander honeycomb buffers under low-velocity impacts through machine learning framework

    10

    confirmed

    Ms. Bianca Omede'

    Politecnico di Milano

    Italy

    2

    15:25

    Nozzle Extension Concept Design of AVIO’s Liquid Rocket Engine

    10

    confirmed

    Dr. Alessandro Lazzari

    AVIO S.p.A.

    Italy

    3

    15:35

    ESTIMATION OF VIBRATION ENVIRONMENT AND STRUCTURAL ASSESSMENT FOR AN EXPERIMENTAL SEMICRYO ROCKET ENGINE

    10

    Mr. Vivek S

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

    India

    4

    15:45

    development of non-detonic separation system – verification of release delay-time effect on lv structures

    10

    confirmed

    Mr. Alessandro Clementi

    AVIO S.p.A.

    Italy

    5

    15:55

    Structural Optimization of a Stiffened Cylinder using Artificial Neural Networks

    10

    confirmed

    Mr. S M SHEHZEB ABBAS

    Pakistan Space and Upper Atmosphere Research Commission (SUPARCO)

    Pakistan

    6

    16:05

    Origami-based tank for geosynchronous refuelling station

    10

    Mr. Romuald Duret

    ISAE-Supaero University of Toulouse

    France

    7

    16:15

    Design Optimization of Satellite Propellant Tank Subjected to Fluid Slosh and Loading Conditions

    10

    Mr. Mustapha Shaibu

    National Space Research and Development Agency (NASRDA), Abuja Nigeria

    Nigeria

    8

    16:25

    Inhouse development of Additive manufactured (AM) Diaphragm Tank for green mono-propellant (GMP) based propulsion system

    10

    confirmed

    Mr. Kuldeep Singh Rajput

    Bellatrix Aerospace Private Limited.

    India

    9

    16:35

    Enhancing the Natural Frequency of Thai Space Consortium-1 Satellite (TSC-1) by Performing an Analysis of Different Structural Configurations and Materials

    10

    confirmed

    Mr. Wichayuth Klankla

    National Astronomical Research Institute of Thailand (NARIT)

    Thailand

    10

    16:45

    An Evaluation of Composite Primary Structure for Habitat Modules

    10

    confirmed

    Mr. Matthew Ziglar

    Boeing Defense Space & Security

    United States

    11

    16:55

    Homeostatic Inflatable Decentralized Autonomous Structures: Intelligent Space Structure Using Inflatable Structure and Decentralized Autonomy

    10

    confirmed

    Prof. Shinichi Kimura

    Tokyo University of Science

    Japan

    12

    17:05

    STEA: A novel tool for Space Thermal Environment Assessment

    10

    confirmed

    Dr. Enrico Friso

    Italy

    13*

    17:15

    Prediction of Thermo-Mechanical State of Reentry Capsule Based on Limited Sensors

    10

    confirmed

    Dr. Jian-Jun Gou

    Northwestern Polytechnical University

    China

    14*

    17:15

    Numerical study of vibration fatigue failure for pipeline welded structure in liquid rocket engines

    10

    confirmed

    Dr. Hanyang Shi

    Xi'an Aerospace Propulsion Institute

    China

    15*

    17:15

    Development and testing of a thrust vector control system for a hybrid rocket engine

    10

    confirmed

    Dr. Olexiy Shynkarenko

    University of Brasilia

    Brazil