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
papers

Order

Time

Paper title

Selection result

Mode

Presentation status

Speaker

Affiliation

Country

1

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

accepted

15'

confirmed

Mr. Zhang Junjie

Aerospace research institute of materials and processing technology (ARIMPT)

China

2

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

accepted

15'

Mr. srinivasa rao

LPSC, ISRO

India

3

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

accepted

15'

Dr. Volodymyr Slyvynskyi

Ukrainian Research Institute of Engineering Technique, OJSC

Ukraine

4

Study of Honeycomb Sandwich Structure for Tank Bearing Load

accepted

15'

confirmed

Mr. Jianwei Wang

Shanghai Institute of Satellite Engineering

China

5

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

accepted

15'

withdrawn

Dr. Anton Kolozeznyy

TSNIIMASH

Russian Federation

6

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

accepted

15'

confirmed

Mr. Qiu Huayong

Aerospace System Engineering Shanghai, China

China

7

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

accepted

15'

confirmed

Dr. Yu Luan

China Academy of Launch Vehicle Technology (CALT)

China

8

An automatic modeling method for POGO system of large liquid rockets

accepted

15'

confirmed

Dr. Shujun Tan

School of Aeronautics and Astronautics, Dalian University of Technology

China

9

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

accepted

15'

confirmed

Mr. YAO Dong

CASC

China

10

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

accepted

15'

Dr. zhang qingya

Beijing Institute of Technology

China

11

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

accepted

15'

confirmed

Prof.Dr. Hyun-Ung Oh

Chosun University

Korea, Republic of