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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

    2017-09-26

    Time

    09:45

    Room

    Panorama Room 2

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

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

    • Rapporteur: Prof. Pierre Rochus, CSL (Centre Spatial de Liège), Belgium;

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    The effects of the center of mass motion on the relative translation and attitude motion of space tugs in close proximity of rendezvous and docking/berthing operations.

    12

    confirmed

    Mr. Luciano Unfried

    Aeronautic Institute of Technology (ITA)

    Brazil

    2

    Towards a European Large Deployable Antenna: Overview of Current Development Activities

    12

    confirmed

    Dr. Thomas Sinn

    HPS GmbH

    Germany

    3

    design, test and comparison of mechanical support principles to increase the robustness of deployable thin-shell cfrp-booms of the deorbiting device adeo

    12

    confirmed

    Mr. Martin Zander

    German Aerospace Center (DLR)

    Germany

    4

    parametric analysis of a controlled deployable space manipulator used for capturing a non-cooperative satellite

    12

    confirmed

    Mr. Angelo Stolfi

    Università di Roma "La Sapienza"

    Italy

    5

    High-Precision Positioning of Reflector Segment by Using Kinematic Couplings for Balloon-Borne Radio Telescope

    12

    confirmed

    Dr. Hiroaki Tanaka

    National Defense Academy

    Japan

    6

    Decrement Properties of Deployment Torque for Self-deployable Tubular CFRP Booms under Stored State

    12

    confirmed

    Mr. Takaomi Chubachi

    Tokyo Institute of Technology

    Japan

    7

    toward a multifunctional interface for future planetary and orbital missions

    12

    confirmed

    Dr. ROBERTO PALAZZETTI

    University of Strathclyde

    United Kingdom

    8

    Design and analysis of bistable composite booms

    12

    withdrawn

    Ms. Orzuri Rique

    Purdue University

    United States

    9

    A Design Method to Keep Asymmetrical Ring Truss Reflector Surface Stable and Test Verification

    12

    confirmed

    Mr. Hui Wang

    China

    10

    Thermo-structural analysis during ascent flight and atmospheric reentry for SARA capsule

    12

    withdrawn

    Dr. ELCIO JERONIMO DE OLIVEIRA

    Institute of Aeronautics and Space (IAE)

    Brazil

    11

    Improvement of Sail Storage Structure and Deployment Mechanism for Next Spin-type Solar Power Sail-craft

    12

    confirmed

    Dr. Osamu Mori

    Japan Aerospace Exploration Agency (JAXA)

    Japan

    12

    Static and dynamic analysis of partially wrinkled membranes for tethered spinning solar sail applications

    12

    confirmed

    Dr. Chao Xu

    Northwestern Polytechnical University

    China

    13

    Passive Nonlinear Actuators for Deploying the Mesh Antennas

    12

    confirmed

    Dr. Zhihua Zhao

    Tsinghua University

    China

    Highly Compressible Origami Bellows for Microgravity Drilling-Debris Containment

    withdrawn

    Mr. Jared Butler

    Brigham Young University

    United States

    *

    Design and Experiment for A High Precision Reflector

    withdrawn

    Dr. XiaoFei Ma

    Xi’an Institute of Space Radio Technology

    China