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  • session 1

    Title

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

    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

    2015-10-12

    Time

    15:15

    Room

    Oranim 1 (ICC, lower level)

    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

    15:15

    CRONUS – Sandwich Common Bulkhead Tank Demonstrator

    12'

    confirmed

    Dr. Carina Ludwig

    MT Aerospace AG

    Germany

    2

    15:27

    Assessment on the failure observed in a liquid fuel tank in an aborted mission of a Geosynchronous vehicle

    12'

    confirmed

    Mr. B Kiran Kumar

    Indian Space Research Organization (ISRO)

    India

    3

    15:39

    the equivalent mechanical model for solving spacecraft large amplitude liquid sloshing problem

    12'

    confirmed

    Ms. Shiping Xing

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

    China

    4

    15:51

    A Theoretical Study on the Structural Loads on the Igniter Hardware of Large Solid Boosters and Proof Pressure Testing Adequacy

    12'

    confirmed

    Mr. Yezhil Arasu

    Vikram Sarabhai Space Centre (VSSC)

    India

    5

    16:03

    Design approach adopted for ensuring the structural integrity of a hydraulic line assembly along the Solid Rocket Motor for a Reusable Launch Vehicle technology Demonstration Mission

    12'

    confirmed

    Mr. Thomas Kurian

    Indian Space Research Organization (ISRO)

    India

    6

    16:15

    sizing of the sandwich dominated structure of the gossamer-1 boom and sail deployment unit using ansys solidshell elements

    12'

    withdrawn

    Mr. Johannes Boblenz

    Deutsches Zentrum fuer Luft- und Raumfahrt (DLR)

    Germany

    7

    16:27

    Design, Simulation and Analysis of Carbon-Fiber Composite and Aluminum Honeycomb Rocket Fins Using Fluid-Structure Interaction for Flutter Analysis

    12'

    confirmed

    Mr. Neil Woodcock

    Concordia University

    Canada

    8

    16:39

    Thermal and mechanical design and test campaign results of a single-piece structure for the URSA MAIOR nanosatellite

    12'

    confirmed

    Dr. Lorenzo Arena

    University of Rome "La Sapienza"

    Italy

    9

    16:51

    Thermal environment generation and verification for on-ground testing of launch vehicle’s fairing

    12'

    no-show

    Dr. Lingling CAO

    Shanghai Academy of Spaceflight Technology (SAST), China Aerospace and Technology Corporation (CASC)

    China

    10

    17:03

    Space qualification tests performed by CIRA on the Alta Hall Effect Electric Thruster HT100D

    12'

    confirmed

    Dr. Vito Salvatore

    CIRA Italian Aerospace Research Center, Capua

    Italy

    11

    17:15

    Optimizing 3-Component Force Sensor Installation for Satellite Force Limited Vibration Testing

    12'

    no-show

    Dr. Carmine Salzano

    United States

    12

    17:27

    Creating a random vibration component test specification for STSAT (Science and Technology Satellite)

    12'

    no-show

    Mr. Talgat Khamitov

    JSC «National Company «Kazakhstan Gharysh Sapary»

    Kazakhstan