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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

    2016-09-27

    Time

    09:45

    Room

    Salon de Eventos 1

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

    PAOLO SANTINI MEMORIAL LECTURE: Half a century of Space Adventure at Centre Spatial of Liège

    30'

    confirmed

    Prof. Pierre Rochus

    CSL (Centre Spatial de Liège)

    Belgium

    2

    DEVELOPMENT OF DIMENSIONALLY STABLE STRUCTURE OF DRAWTUBE OF OPTICAL DEVICE OF COMPOSITE MATERIAL

    15'

    confirmed

    Ms. Antonina Kulik

    Yuzhnoye State Design Office

    Ukraine

    3

    Verification Testing of the Gossamer-1 Deployment Demonstrator

    15'

    no-show

    Mr. Jan Thimo Grundmann

    Deutsches Zentrum für Luft- und Raumfahrt e.V. (DLR)

    Germany

    4

    impedance control of a multi-arm space robot for capturing a non-cooperative target

    15'

    no-show

    Mr. Angelo Stolfi

    Università di Roma "La Sapienza"

    Italy

    5

    A High-accuracy Micro-deformation Measurement Method for High-resolution Space Camera Complex Structured

    15'

    no-show

    Dr. Li JIANG

    China Academy of Launch Vehicle Technology (CALT)

    China

    6

    The research of the vibration reliability of the ceramic packaging BGA and CGA devices

    15'

    withdrawn

    Dr. Wei Zhang

    China Academy of Launch Vehicle Technology(CALT)

    China

    7

    Attitude and vibration control of a satellite containing flexible solar arrays by using reaction wheels, thrusters, and piezoelectric transducers as sensors and actuators.

    15'

    confirmed

    Dr. Ijar M. Da Fonseca

    ITA-DCTA

    Brazil

    8

    Ground Experiments of Boom-membrane Integrated Deployable Structures for Micro Satellites

    15'

    withdrawn

    Prof. Hiroshi Furuya

    Tokyo Institute of Technology

    Japan

    9

    A Modular and Efficient System for Antenna Deployment in Swayam: A Platform for Reliable Bi- Directional Communication

    15'

    withdrawn

    Ms. Tanvi Katke

    College of Engineering, Pune

    India

    10

    a study on the asymmetric spinning deployment of membrane structure with variation thickness

    15'

    confirmed

    Mr. Hiroyuki Kinoshita

    Tokai University

    Japan

    11

    Design and ground test of the isolator for satellite attitude control actuator

    15'

    confirmed

    Mr. Jia Tian

    China Academy of Space Technology (Xi’an), CAST

    China

    12

    FBG optical sensors for environmental tests of microsatellites

    15'

    confirmed

    Dr. Giampiero Sindoni

    Sapienza University of Rome

    Italy

    13

    Topology optimization and FDM prototyping of bionic inspired strengthening-ribs in membranes of spacecraft

    15'

    confirmed

    Prof. Qingxi Hu

    Shanghai University

    China