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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

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    15:15

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

    15'

    confirmed

    Mr. Zhang Junjie

    Aerospace research institute of materials and processing technology (ARIMPT)

    China

    2

    15:30

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

    15'

    Mr. srinivasa rao

    LPSC, ISRO

    India

    3

    15:45

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

    15'

    Dr. Volodymyr Slyvynskyi

    Ukrainian Research Institute of Engineering Technique, OJSC

    Ukraine

    4

    16:00

    Study of Honeycomb Sandwich Structure for Tank Bearing Load

    15'

    confirmed

    Mr. Jianwei Wang

    Shanghai Institute of Satellite Engineering

    China

    5

    16:15

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

    15'

    withdrawn

    Dr. Anton Kolozeznyy

    TSNIIMASH

    Russian Federation

    6

    16:30

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

    15'

    confirmed

    Mr. Qiu Huayong

    Aerospace System Engineering Shanghai, China

    China

    7

    16:45

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

    15'

    confirmed

    Dr. Yu Luan

    China Academy of Launch Vehicle Technology (CALT)

    China

    8

    17:00

    An automatic modeling method for POGO system of large liquid rockets

    15'

    confirmed

    Dr. Shujun Tan

    School of Aeronautics and Astronautics, Dalian University of Technology

    China

    9

    17:15

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

    15'

    confirmed

    Mr. YAO Dong

    CASC

    China

    10

    17:30

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

    15'

    Dr. zhang qingya

    Beijing Institute of Technology

    China

    11

    17:45

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

    15'

    confirmed

    Prof.Dr. Hyun-Ung Oh

    Chosun University

    Korea, Republic of