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  • session 2

    Title

    Space Structures II - Development and Verification (Deployable and Dimensionally Stable Structures)

    type

    oral

    Description

    The topics to be addressed include evaluation of analysis versus test results for deployable and dimensionally stable structures, e.g. reflectors, telescopes, antennas; examination of both on-ground and in-orbit testing, thermal distortion and shape control, structural design, development and verification; lessons learned.

    Date

    2021-10-26

    Time

    09:45

    Room

    Rais Al Khaimah

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

    • Co-Chair: Dr. Oliver Kunz, Beyond Gravity, Switzerland;

    • Rapporteur: Mr. Aicke Patzelt, MT Aerospace AG, Germany;

    • Rapporteur: Mr. Thomas Sinn, DcubeD (Deployables Cubed GmbH), Germany;

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    09:45

    Global/local and advanced multi-scale simulation of composite TRAC booms

    10

    confirmed

    Dr. Alfonso Pagani

    Politecnico di Torino

    Italy

    4

    09:55

    An attitude/spin control architecture for a spacecraft equipped with a flexible rotating payload based on Model Predictive Control

    10

    confirmed

    Mr. Paolo Iannelli

    Sapienza University of Rome

    Italy

    6

    10:05

    Power Cube: Applications, Design, Breadboarding and Roadmap of a 1U deployable 100W NanoSat Solar Array

    10

    confirmed

    Dr. Thomas Sinn

    DcubeD (Deployables Cubed GmbH)

    Germany

    11

    10:15

    Experimental Validation of Deployable Tape Spring Hinge Embedded with Surperplastic Shape Memory Alloy

    10

    confirmed

    Prof.Dr. Hyun-Ung Oh

    Chosun University

    Korea, Republic of

    1002

    10:25

    Effects of Structural Configurations On Deployment Behavior of Two-Dimensional Self-Deployable Structure with Corrugated Panels

    10

    confirmed

    Mr. Makoto Yoshioka

    Tokyo Institute of Technology

    Japan

    1003

    10:35

    DETERMINING THE BREAKING LOAD OF SMOOTH SPHERICAL AND CONICAL TANKS USING THE METHOD OF COMPUTATIONAL EXPERIMENTS

    10

    confirmed

    Mr. Volodymyr Baburov

    Yuzhnoye State Design Office

    Ukraine

    1005

    10:45

    Wrap-rib Antenna Deployment Analysis by Rayleigh Ritz Method

    10

    confirmed

    Prof. Tetsuo Yasaka

    Institute for Q-shu Pioneer of Space, Inc. (iQPS)

    Japan

    1007

    10:55

    deployment and stretching of the circular solar sail by a superconducting current loop

    10

    Prof. Roman Ya. Kezerashvili

    New York City College of Technology, The City University of New York

    United States

    1008

    11:05

    Deployment Simulation of Solar Sail with Rotationally Skew Folding : parametric analysis by deployment structure configuration

    10

    confirmed

    Mr. Shuhei Yamada

    University of Tokyo

    Japan

    1009

    11:15

    Manufacturing and testing of a telescope for small satellites using CFRP booms

    10

    Mr. Gianluca De Zanet

    University of Surrey

    United Kingdom

    1010

    11:25

    Comparative Study of Non-linear Analysis Tools for Release Simulations of Clampband-joint Separation Systems

    10

    confirmed

    Ms. Antonia Grethen-Bußmann

    Luleå University of Technology

    Sweden

    1012

    11:35

    on-orbit manufacturing of large space structures using solid foams

    10

    confirmed

    Mr. Peter G.B. Hastie

    University of Glasgow

    United Kingdom