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    Title

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

    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

    2013-09-24

    Time

    09:45

    Room

    306B

    IPC members
    • Chairman: Prof. Paolo Gasbarri, Sapienza University of Rome, Italy;

    • Chairman: Mr. Jean-Alain Massoni, Thales Alenia Space France, France;

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

    papers

    Order

    Presentation status

    Mode

    Paper title

    Speaker

    Affiliation

    Country

    1

    confirmed

    30'

    KEYNOTE LECTURE: Space Structure – Yesterday, Today and Tomorrow

    Prof. Tetsuo Yasaka

    QPS Institute

    Japan

    2

    confirmed

    15'

    A New Approach to Stabilization of Inflatable Space Structures

    Mr. Manpreet Puri

    University of Strathclyde

    United Kingdom

    3

    confirmed

    15'

    On-orbit experimental results of the REX-J extendable robotic manipulator

    Mr. Atsushi Ueta

    Japan Aerospace Exploration Agency (JAXA)

    Japan

    4

    confirmed

    15'

    Characterizing Lightweight and Dimensionally Ultra Stable Structures for Space Application

    Mr. Ruven Spannagel

    DLR, German Aerospace Center

    Germany

    5

    withdrawn

    15'

    Thermal property and microstructure contrast of three kinds of carbon/silicon carbide composites

    Dr. Jin Li

    China Aerospace Science and Technology Corporation (CASC)

    China

    6

    confirmed

    15'

    Deployment analysis and control strategies of flexible space manipulators

    Mr. Andrea Pisculli

    University of Rome "La Sapienza"

    Italy

    7

    withdrawn

    15'

    Multibody analysis of a two axis oriented deployable Solar Array

    Mrs. Anne GIOVANNINI

    Thales Alenia Space France

    France

    8

    confirmed

    15'

    Design and evaluation of inflatable structural concepts for aerodynamic drag augmentation.

    Mr. Gabriel Secheli

    Surrey Space Centre, University of Surrey

    United Kingdom

    9

    confirmed

    15'

    Shape Measurement of Creased Large Space Membrane by Photometric Stereo Technique

    Prof. Hiroshi Furuya

    Tokyo Institute of Technology

    Japan

    10

    confirmed

    15'

    Equivalent Stiffness of Large Deployable Membrane with Random Initial Deformation

    Ms. Ayumu Yamasaki

    Tokyo Institute of Technology

    Japan

    11

    confirmed

    15'

    Parametric Study of Flexible Solar Array Based on Orthogonal Method

    Dr. Liu Dali

    Aerospace System Engineering Shanghai

    China

    12

    confirmed

    15'

    Minimum Weight Design of Orthotropic Cylindrical Launcher Shell Structures subjected to Local Load Introduction

    Dr. Jochen Albus

    Airbus DS GmbH

    Germany

    NUMERICAL SIMULATION OF FOLDING AND DEPLOYING PROCESS OF LENTICULAR COLLAPSIBLE COMPOSITE BOOMS

    Dr. Guangqiang Fang

    Aerospace System Engineering Shanghai

    China