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  • session 2

    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, University of Rome “La Sapienza”, Italy;

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

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

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    KEYNOTE LECTURE: Space Structure – Yesterday, Today and Tomorrow

    30'

    confirmed

    Prof. Tetsuo Yasaka

    QPS Institute

    Japan

    2

    A New Approach to Stabilization of Inflatable Space Structures

    15'

    confirmed

    Mr. Manpreet Puri

    University of Strathclyde

    United Kingdom

    3

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

    15'

    confirmed

    Mr. Atsushi Ueta

    Japan Aerospace Exploration Agency (JAXA)

    Japan

    4

    Characterizing Lightweight and Dimensionally Ultra Stable Structures for Space Application

    15'

    confirmed

    Mr. Ruven Spannagel

    DLR, German Aerospace Center

    Germany

    5

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

    15'

    withdrawn

    Dr. Jin Li

    China Aerospace Science and Technology Corporation (CASC)

    China

    6

    Deployment analysis and control strategies of flexible space manipulators

    15'

    confirmed

    Mr. Andrea Pisculli

    University of Rome "La Sapienza"

    Italy

    7

    Multibody analysis of a two axis oriented deployable Solar Array

    15'

    withdrawn

    Mrs. Anne GIOVANNINI

    Thales Alenia Space France

    France

    8

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

    15'

    confirmed

    Mr. Gabriel Secheli

    Surrey Space Centre, University of Surrey

    United Kingdom

    9

    Shape Measurement of Creased Large Space Membrane by Photometric Stereo Technique

    15'

    confirmed

    Prof. Hiroshi Furuya

    Tokyo Institute of Technology

    Japan

    10

    Equivalent Stiffness of Large Deployable Membrane with Random Initial Deformation

    15'

    confirmed

    Ms. Ayumu Yamasaki

    Tokyo Institute of Technology

    Japan

    11

    Parametric Study of Flexible Solar Array Based on Orthogonal Method

    15'

    confirmed

    Dr. Liu Dali

    Aerospace System Engineering Shanghai

    China

    12

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

    15'

    confirmed

    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