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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

    2013-09-23

    Time

    15:15

    Room

    306B

    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

    Presentation status

    Mode

    Paper title

    Speaker

    Affiliation

    Country

    1

    confirmed

    15'

    Analyzing the fractal of the fracture of welding joint in aerospace industry to evaluate the fracture toughness

    Mr. Zhang Junjie

    Aerospace research institute of materials and processing technology (ARIMPT)

    China

    2

    15'

    development and demonstration of friction stir welding process towards realisation of propellant tanks for space programme

    Mr. srinivasa rao

    LPSC, ISRO

    India

    3

    15'

    New possibilities in creating of effective composite size-stable honeycomb structures designed for space purposes

    Dr. Volodymyr Slyvynskyi

    Ukrainian Research Institute of Engineering Technique, OJSC

    Ukraine

    4

    confirmed

    15'

    Study of Honeycomb Sandwich Structure for Tank Bearing Load

    Mr. Jianwei Wang

    Shanghai Institute of Satellite Engineering

    China

    5

    withdrawn

    15'

    Thermo mechanical architecture development of liquid hydrogen tanks for upper stages with use of cryogenic helium machine

    Dr. Anton Kolozeznyy

    TSNIIMASH

    Russian Federation

    6

    confirmed

    15'

    The Development History And Application Status Of China’s Manned Spacecraft Docking Mechanism

    Mr. Qiu Huayong

    Aerospace System Engineering Shanghai, China

    China

    7

    confirmed

    15'

    dynamic analysis and validation for rotating separation of lm-5's large-scale payload fairing

    Dr. Yu Luan

    China Academy of Launch Vehicle Technology (CALT)

    China

    8

    confirmed

    15'

    An automatic modeling method for POGO system of large liquid rockets

    Dr. Shujun Tan

    School of Aeronautics and Astronautics, Dalian University of Technology

    China

    9

    confirmed

    15'

    inverse estimation on elastic parameter of particulate reinforced composites based on cax

    Mr. YAO Dong

    CASC

    China

    10

    15'

    Analysis on carbon-carbon nozzle thermal stress of solid rocket motors

    Dr. zhang qingya

    Beijing Institute of Technology

    China

    11

    confirmed

    15'

    Performance Investigation of Spaceborne Micro-vibration Isolation System Combined with Heat Pipe Cooling System

    Prof.Dr. Hyun-Ung Oh

    Chosun University

    Korea, Republic of