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  • session 1

    Title

    Space Structures 1 - 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

    2012-10-01

    Time

    15:15

    Room

    TS07 (Sala Regulus, Hall 3)

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

    • Chairman: Dr. Andreas Rittweger, DLR (German Aerospace Center), Germany;

    • Rapporteur: Mr. Jean-Alain Massoni, Thales Alenia Space France, France;

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    Simulation Of Vega Dynamic environment By Using Propellant Complex Characterization

    15'

    confirmed

    2

    Design of a COPV for liquid storable propellants of 4th stage VEGA launcher

    15'

    confirmed

    Mr. andrea mataloni

    AVIO Propulsione Aerospaziale

    Italy

    3

    Practical application of DIC in Fatigue and Fracture Toughness Testing

    15'

    confirmed

    Mr. Fawad Tariq

    Pakistan Space and Upper Atmosphere Research Commission (SUPARCO)

    Pakistan

    4

    A research on shock prediction method correlated with FORMOSAT-2 satellite pyro-shock test results

    15'

    confirmed

    Mr. Chi-Wei Chou

    Taiwan, China

    5

    Development of a structural model for Korean lunar explorer

    15'

    withdrawn

    Mr. Taek-Joon Son

    Korean Air

    Korea, Republic of

    6

    Standard FEM validation checks and quality of response prediction

    15'

    confirmed

    Dr. Guglielmo Aglietti

    University of Southampton

    United Kingdom

    7

    Analysis of process-induced deformation of complicated composite curved surface

    15'

    withdrawn

    Mr. Yizhi Fu

    Beihang University

    China

    8

    Novel technologies and new methodology for measuring the contamination of (semi) volatile organic compounds from materials and environments.

    15'

    no-show

    Dr. Caroline Widdowson

    United Kingdom

    9

    Post-Flight Analysis of the Recovered Hayabusa Heatshield and Results from Airborne Observation

    15'

    confirmed

    Dr. Tetsuya Yamada

    ISAS&JSPEC/JAXA

    Japan

    10

    Instrumentation of the EXPERT flap for Wind Tunnel Testing and Evaluation of Test Results

    15'

    confirmed

    Mr. Thomas Thiele

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

    Germany

    11

    Experimental Investigation of the Emissivity of the EXPERT Flap in SCIROCCO Plasma Wind Tunnel Tests

    15'

    confirmed

    Dr. Carlo Purpura

    CIRA Italian Aerospace Research Centre

    Italy

    12

    Design Considerations for Solid Rocket Booster Flex Nozzle Hardware

    15'

    withdrawn

    Mr. Atha Ur Rahman Khan

    Indian Space Research Organization (ISRO)

    India

    13

    VV01 - LARES System development and verification

    Poster

    confirmed

    Mr. Alessandro Bursi

    OHB Italia SpA

    Italy

    14

    Prediction of Transient Skin Temperature of High Speed Vehicles through CFD

    Poster

    withdrawn

    Dr. Mukkarum Husain

    Pakistan

    15

    Nonlinear feedback composite control of space manipulator system with bounded torque inputs and uncertain parameters

    Poster

    confirmed

    Dr. Jie Liang

    China

    16

    Thermo-structural design of ultra high temperature ceramic (UHTC) winglets of a re-entry space vehicle

    Poster

    confirmed

    Dr. ROBERTO SCIGLIANO

    CIRA Italian Aerospace Research Centre

    Italy

    17

    Qualification tests on the optical retro-reflectors of LARES satellite.

    Poster

    confirmed

    Prof. Antonio Paolozzi

    Sapienza University of Rome

    Italy

    18

    OPTIMIZATION OF MARTIAN REGOLITH AND ULTRA-HIGH MOLECULAR WEIGHT POLYETHYLENE COMPOSITES FOR RADIATION SHIELDING AND HABITAT STRUCTURES

    Poster

    Ms. Milan Barnett

    United States