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  • session 1

    Title

    Space Structures I - Development and Verification (Space Vehicles and Components)

    type

    oral

    Description

    The topics to be addressed include evaluation of analysis versus test results, spacecraft and launch vehicles system and subsystems, e.g. pressurised structures, tanks, loads introduction, primary structures, fluidic equipment, control surfaces; examination of both on-ground and in-orbit testing, launch dynamic environment as related to structural design, space vehicles development and launch verification such as sine, random and acoustic vibration testing and lessons learned.

    Date

    2017-09-25

    Time

    15:15

    Room

    Panorama Room 2

    IPC members
    • Co-Chair: Mr. Alwin Eisenmann, IABG Industrieanlagen - Betriebsgesellschaft mbH, Germany;

    • Co-Chair: Dr. Andreas Rittweger, DLR (German Aerospace Center), Germany;

    • Rapporteur: Dr. Jochen Albus, ArianeGroup, Germany;

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    Verification and Ground Qualification Approach for the Structure of the ORION-MPCV European Service Module

    12

    confirmed

    Dr. Gandolfo Di Vita

    ESA

    The Netherlands

    2

    Using Virtual Testing as pre- and post- test tool for spacecraft vibration testing

    12

    confirmed

    Dr. Marcello Remedia

    Surrey Space Centre, University of Surrey

    United Kingdom

    3

    Wireless and Batteryless Vibration Testing of Space Structures with Implanted LSI Sensors

    12

    confirmed

    Mr. Nitish Rajoria

    Keio University

    Japan

    4

    A NEW CONCEPT IN VIRTUAL SIMULATION OF A SPACE STRUCTURE VIBRATION TEST

    12'

    no-show

    Mr. Vincenzo Di Pietro

    Thales Alenia Space Italia (TAS-I)

    Italy

    5

    Design Strategy, Numerical Analysis and Testing of a Modular Satellite Structure

    12

    confirmed

    Mr. Thomas A. Schervan

    RWTH Aachen University

    Germany

    6

    ESTCube-2 structure development, analysis, testing and verification

    12

    confirmed

    Mr. Iaroslav Iakubivskyi

    University of Tartu

    Estonia

    7

    optimization for structure system of micro-satellite

    12'

    no-show

    Mr. Liming Fan

    School of Astronautics, Beihang University, Beijing 100191, PR China

    China

    8

    formosat-5 satellite structure development and dynamic launch environment verification

    12

    confirmed

    Mr. Jen-Chueh KUO

    National Space Organization

    Taiwan, China

    9

    Research on column buckling under internal pressure of plane-cone shaped metal bellows

    12

    confirmed

    Mr. Muye Chen

    Beijing institute of Astronautical Systems Engineering, Beijing

    China

    10

    Multidisciplinary Design Optimization of a Satellite Structure by Additive Manufacturing

    12

    confirmed

    Mr. Marius Bierdel

    Fraunhofer EMI

    Germany

    11

    On-ground testing of a restraint layer for inflatable modules for lunar orbital application

    12

    confirmed

    Dr. Anton Kolozeznyy

    TSNIIMASH

    Russian Federation

    12

    A study on the Design and structural analysis of filament wound Composite Motor case with Inter metallic segment joint

    12

    confirmed

    Mr. Paul Murugan J

    Indian Space Research Organization (ISRO)

    India

    13

    Verification of Diaphragm Analysis

    12

    confirmed

    Mr. Stefan Weiland

    MT Aerospace AG

    Germany