session 1

Title: Space Structures I - Development and Verification (Space Vehicles and Components)
Description: The following topics will be included: Analysis versus test results for spacecraft, launch vehicles and their components (e.g. pressurized structures, tanks, load introductions, primary structures, fluidic equipment, control surfaces); examination of both on-ground and in-orbit testing, launch dynamic environments as related to structural design, development and verification, such as sine, random and acoustic vibration and lessons learned.
Date: 2008-09-29
Time: 15:00
Room: Dochart 1

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	Paper title	Mode	Speaker	Affiliation	Country
1	development progress on cmc torque actuated control surfaces by re-entry verification test	presentation	Dr. Harald Lange	MT Aerospace AG	Germany
2	Optimization of stiffened cylindrical shell of propellant tanks	presentation	Mr. HUANG CHENG	CASC	China
3	study on phased array ultrasonic nondestructive testing for aluminum alloy friction stir welding	presentation	Mrs. leena zhang		China
4	Structural Design and Analysis of an Advanced LEO EO Satellite/STM	presentation	Dr. Jae Hyuk Lim	Korea Aerospace Research Institute (KARI)	Korea, Republic of
5	Design and Development of Polymer-Lined Composite Tank for Liquid Hydrogen Propellant of Reusable Vehicle	presentation	Dr. Shinsuke Takeuchi	Japan Aerospace Exploration Agency (JAXA)	Japan
6	research on sound absorption properties of variable aperture micro-perforated panel in spacecraft	presentation	Mr. Linling Li	CAST	China
7	random fatigue life prediction due to vibro-acoustic and thermal environments	presentation	Mr. Pietro Carlo Marucchi Chierro	Thales Alenia Space Italia	Italy
8	Study of a coupling mechanism between two bodies at high temperature values	presentation	Dr. Michele Ferraiuolo	C.I.R.A. - S.C.P.A.	Italy
9	three-element mesh size criterion and its application to random vibration analysis of electronic equipment of satellite	presentation	Prof. Yueyu Wang	China Academy of Space Technology (CAST)	China
10	finite element analysis on the progressive delamination process of laminates based on self-adapting delamination element method	presentation	Mr. Lipeng Wang	China Academy of Launch Vehicle Technology (CALT)	China
11	Neuro-fuzzy modeling for forecasting future dynamical behaviors of vibration testing in satellites qualification	presentation	Dr. Ernesto Araujo	Instituto Nacional de Pesquisas Espaciais (INPE)	Brazil
12	Choice of materials and design of propellant tanks and adjacent structures for future launchers, including RLV	discussion	Mr. Yuriy Gusev	TSNIIMASH	Russian Federation
13	scientific fundamentals of efficient adhesive joint in honeycomb structures for aerospace applications	discussion	Dr. Volodymyr Slyvynskyi	Ukrainian Research Institute of Engineering Technique, OJSC	Ukraine

session 1

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