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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

    2014-09-29

    Time

    15:15

    Room

    713A

    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

    The THOR Space Station at EML2: analysis and preliminary design an innovative adaptable docking system.

    12'

    confirmed

    Prof. Stéphanie Lizy-Destrez

    SUPAERO- Ecole Nationale Supérieure de l'Aéronautique et de l'Espace

    France

    2

    verification and validation for the thermo-mechanical design of ultra high temperature ceramic (uhtc) winglets of a re-entry space vehicle

    12'

    confirmed

    Dr. ROBERTO SCIGLIANO

    CIRA Italian Aerospace Research Centre

    Italy

    4

    Space qualification test of vibration isolator for low amplitude vibration

    12'

    confirmed

    Mr. Geeyong Park

    Korea Advanced Institute of Science and Technology (KAIST)

    Korea, Republic of

    5

    METHOD OF WEIGHT OPTIMIZATION OF DISCRETELY LOADED ROCKET BAYS OF WAFFLE STRUCTURE

    12'

    no-show

    Mr. Vitaliy Danchenko

    Yuzhnoye State Design Office

    Ukraine

    6

    Acoustic performance of foam filled honeycomb sandwich structures

    12'

    withdrawn

    Dr. R. Ramesh Kumar

    Indian Space Research Organization (ISRO)

    India

    7

    development of a metal corrugated diaphragm tank for use in liquid bipropellant propulsion systems

    12'

    no-show

    Dr. Fei Yan

    Shanghai Institute of Space Propulsion

    China

    8

    Equivalent Stiffness Approach (ESAF) for Two Dimensional Analysis of Flanged Joints of Solid Rocket Motors

    12'

    no-show

    Mr. Sri S. Somanath

    Vikram Sarabhai Space Centre (VSSC)

    India

    9

    analysis method of structural fracture behavior

    12'

    no-show

    Mr. Xibo Wang

    Beijing Institute of Aerospace Systems Engineering, China Aerospace Science and Technology Corporation (CASC)

    China

    10

    robust tracking control of dual-arm flexible joint space robot based on backstepping technology

    12'

    no-show

    Dr. Jie Liang

    China

    12

    performance investigation of solid and solid-grease hybrid lubricated harmonic drive gears under thermal-vacuum environment

    12'

    confirmed

    Prof. hui zhou

    China Academy of Space Technology (CAST)

    China

    12

    The Satellite Topology Optimization of Truss Structure and Its Size Sensitivity Analysis

    12'

    confirmed

    Mr. Huang Fan

    Shanghai Institute of Satellite Engineering

    China

    13

    Lateral-staging space launch vehicles dynamics with allowance for propellant crossfeed

    12'

    withdrawn

    Mr. Arseniy Pavlov

    Bauman Moscow State Technical University

    Russian Federation