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. pressurized 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: 2010-09-27
Time: 15:15
Room: Meeting Room 42

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	Presentation status	Speaker	Affiliation	Country
1	key cryogenic technologies enhancement and verifications within hxg macro demonstrator	10	confirmed	Dr. Yves PREL	Centre National d'Etudes Spatiales (CNES)	France
2	Development and Verification of Polymer-Lined Composite Liquid Hydrogen Tank for Reusable Vehicle	10	confirmed	Dr. Shinsuke Takeuchi	Japan Aerospace Exploration Agency (JAXA)	Japan
3	development of propellant tank Structure for Korea space launch vehicle	10	confirmed	Dr. Yeong-Moo Yi	Korea Aerospace Research Institute (KARI)	Korea, Republic of
4	Structural load test programme for LVM3: Test Configurations and Lessons learned.	10		Mr. Somanath Sreedhara Panicker	Indian Space Research Organization (ISRO)	India
5	Design, Realisation and Testing of A Large Diameter Solid Booster Motor Case	10	withdrawn	Mr. Thomas Kurian	Indian Space Research Organization (ISRO)	India
6	Advanced Structural Analysis of Flex Nozzle for Solid Rocket Booster	10	confirmed	Mr. Yezhil Arasu	Vikram Sarabhai Space Centre (VSSC)	India
7	Structural analysis and preliminary space characterization of a prototype hollow laser retroreflector.	10	confirmed	Dr. Claudio Cantone	Istituto Nazionale di Fisica Nucleare (INFN)	Italy
8	A strategy for finite element model verification of complex spacecraft	10	confirmed	Dr. Jifeng Ding	China Academy of Space Technology (CAST)	China
9	A notching method for random vibration acceleration spectra derived from the force limiting technique	10	confirmed	Dr. Yuanjie Zou	China Academy of Space Technology (CAST)	China
10	Low Shock Non-Pyro Separation System for Small Satellite from Launch Vehicle	10	withdrawn	Mr. Seiya Nagano	Kyushu University	Japan
11	Structural Analysis and Verification of a Recovery Subsystem for the Atmospheric Reentry Satellite	10		Mr. Artur C. Arantes-Filho	Instituto de Aeronáutica e Espaço (IAE)	Brazil
12	technical study on the structural design of korean lunar explorer	10	confirmed	Mr. Sun-Won Kim	Korea Aerospace Research Institute (KARI)	Korea, Republic of
13	Development of the accelerometer sensor heads for the GOCE satellite: Assessment of the critical items and qualification	10	confirmed	Dr. Guillaume Bodoville	Office National d’Etudes et de Recherches Aérospatiales (ONERA)	France
14	Optimization and Thermal Control of a multi-layered structure for space electronic device	10	confirmed	Dr. Riccardo Monti	Sapienza University of Rome	Italy

session 1

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