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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

    2015-10-13

    Time

    09:45

    Room

    Oranim 1 (ICC, lower level)

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

    • Co-Chair: 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

    design and analysis of a composite sandwich solar array structure for the eu:cropis compact satellite with as few release mechanisms as possible

    12'

    confirmed

    Mr. Thilo Glaser

    German Aerospace Center (DLR)

    Germany

    2

    Development of calculation model of large-size thermo-dimensionally stable structure of composite materials

    12'

    confirmed

    Mr. Serhii Kushnirenko

    Yuzhnoye State Design Office

    Ukraine

    3

    Development of Elastic Forces Model for High Area-to-Mass Ratio Flexible Spacecraft

    12'

    withdrawn

    Mr. Dayu ZHANG

    National Key Laboratory of Aerospace Flight Dynamics,Northwestern Polytechnical University,Xi'an,

    China

    4

    Environmental Testing and Analysis of a Boom Deployment Mechanism for GOSSAMER-2

    12'

    confirmed

    Mr. Sebastian Meyer

    German Aerospace Center (DLR)

    Germany

    5

    Deployment and Post Grasping Issues for a Light Weight Robotic Arm Mounted on a Small Space-Services

    12'

    confirmed

    Prof. Paolo Gasbarri

    Università di Roma "La Sapienza"

    Italy

    6

    mechanical characterization of deployable thin shell cfrp-booms for the cubeSat “de-orbit sail”

    12'

    confirmed

    Mr. Martin Zander

    German Aerospace Center (DLR)

    Germany

    7

    AstroTube Max: The development and testing of a low mass extendible CFRP telescopic boom for satellite applications.

    12'

    confirmed

    Mr. Vincent Fraux

    Oxford Space Systems

    United Kingdom

    8

    use of composite materials based on cyanate ester resins for manufacture of space qualified structures with high dimentional stability

    12'

    confirmed

    Dr. Gabriel Sznejer

    Rafael Advanced Defense Systems Ltd.

    Israel

    9

    ground testing of a 8-meter 4-quadrant scalable solar sail

    12'

    confirmed

    Dr. Xinghua Zhang

    Qian Xuesen Laboratory of Space Technology

    China

    10

    Thermal deformation on laser retro-reflectors of LARES satellite

    12'

    confirmed

    Prof. Antonio Paolozzi

    Sapienza University of Rome

    Italy

    11

    Model and analysis of bi-hoop circular deployable truss

    12'

    withdrawn

    Prof.Dr. Minger Wu

    Tongji University

    China