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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

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

    • Co-Chair: Dr. Andreas Rittweger, DLR (German Aerospace Center), Germany;

    • Rapporteur: Dr. Jochen Albus, ArianeGroup, Germany;

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    Analyzing Quasi-Static and Dynamic Responses of a 3U Cubesat Structure during Launching

    10

    confirmed

    Ms. Ruqayya Alhammadi

    Khalifa University of Science and Technology (KUST)

    United Arab Emirates

    2

    Engineering challenges in configuring a modular cryogenic upper stage

    10

    confirmed

    Mr. Sunil M

    Liquid Propulsion System centre

    India

    5

    Numerical and experimental study for the burst pressure evaluation of polyimide pipelines used in cryogenic rocket stages for optimal design

    10

    confirmed

    Mr. Vivek S

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

    India

    8

    Dynamic Response and Behavior Simulation of a Thermal Boot Employed in a Heavy Lift Launch Vehicle

    10

    confirmed

    Mr. Mohit Agarwal

    Indian Space Research Organization (ISRO)

    India

    10

    Temperature estimate of LARES 2 satellite

    10

    confirmed

    Mr. Khaja Faisal Hussain

    Scuola di Ingegneria Aerospaziale "La Sapienza"

    Italy

    11

    Thermal Analysis of Hybrid System Combined with Thin Film and Bulk Structure for Solar Power Satellite

    10

    confirmed

    Mr. Takaya Nakamura

    Tokyo University of Science

    Japan

    14

    Impact Force Calculation Using Non-smooth DEM and Consideration of Landing Contact Surface Shape of Landing Leg for Small Mars Lander

    10

    confirmed

    Ms. Shiori Matsumoto

    Aoyama Gakuin University

    Japan