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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

    2021-10-25

    Time

    15:15

    Room

    Rais Al Khaimah

    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

    15:15

    Thermal Vacuum and Balance Test Method and Validation on Optical Payload

    10

    confirmed

    Mr. Mohamed Alsalami

    Mohammed Bin Rashid Space Centre (MBRSC)

    United Arab Emirates

    4

    15:25

    Sierra Nevada Corporation's LIFE Softgoods Certification

    10

    confirmed

    Mr. Jeffrey Valania

    Sierra Space

    United States

    7

    15:35

    A global-local approach for the free-edge analysis of composite structures under thermal loads

    10

    confirmed

    Dr. Enrico Zappino

    Politecnico di Torino

    Italy

    8

    15:45

    Thermal insulation foam for the high precision thermal modeling of space satellites

    10

    confirmed

    Mr. Nikolay Mullin

    Skolkovo Institute of Science and Technology

    Russian Federation

    11

    15:55

    On the vibration testing of space structures

    10

    withdrawn

    Dr. Nikolay Asmolovskiy

    Space Structures GmbH

    Germany

    12

    16:05

    Design and Qualification of a Lightweight Payload Module Optimized for Payload and AIT Flexibility

    10

    confirmed

    Mr. Thomas A. Schervan

    RWTH Aachen University

    Germany

    1002

    16:15

    Radiation Hardness Testing of CubeSat Solar Panels using the parasitic fast neutrons produced at PETtrace 800 Medical Cyclotron

    10

    confirmed

    Dr. Bhaskar Mukherjee

    The University of Sydney

    Australia

    1003

    16:25

    structure modelling and optimal configuration of a microsatellite in equatorial orbit

    10

    confirmed

    Mr. Poki Agung Budiantoro

    Indonesian Space Agency Secretariat (INASA)

    Indonesia

    1005

    16:35

    The development of a cryogenic propellant tank fully made of composite materials

    10

    confirmed

    Mr. Pavlo Galagan

    Yuzhnoye State Design Office

    Ukraine

    1006

    16:45

    Cross-longitudinal reinforcement design for thin structures in aerospace inspired by dragonfly wing

    10

    confirmed

    Mr. Hiroki Kawabe

    The University of TOKYO, Graduate school

    Japan

    1009

    16:55

    evaluation of shape and solar radiation torque of boom extendable membrane structure with devices

    10

    confirmed

    Ms. Ayaka Fujita

    Tokai University

    Japan

    1010

    17:05

    Flight tests of 3D-printed high thermal conductivity parts due to the phase-changes heat pipe similar structures in the inner cavities

    10

    withdrawn

    Mr. Nikolay Mullin

    Skolkovo Institute of Science and Technology

    Russian Federation

    *

    Aerothermal analysis and thermal protection of grid fins for reentry rockets

    Dr. Liang CHEN

    Beijing Interstellar Glory Space Technology Co., Ltd

    China