session 1

Title: Space Structures I - Development and Verification (Space Vehicles and Components)
type: oral
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: 2017-09-25
Time: 15:15
Room: Panorama Room 2

IPC members

Co-Chair: Mr. Alwin Eisenmann, IABG Industrieanlagen - Betriebsgesellschaft mbH, Germany;
Co-Chair: Dr. Andreas Rittweger, DLR (German Aerospace Center), Germany;
Rapporteur: Dr. Jochen Albus, ArianeGroup, Germany;

papers
Order	Paper title	Mode	Presentation status	Speaker	Affiliation	Country
1	Verification and Ground Qualification Approach for the Structure of the ORION-MPCV European Service Module	12	confirmed	Dr. Gandolfo Di Vita	ESA	The Netherlands
2	Using Virtual Testing as pre- and post- test tool for spacecraft vibration testing	12	confirmed	Dr. Marcello Remedia	Surrey Space Centre, University of Surrey	United Kingdom
3	Wireless and Batteryless Vibration Testing of Space Structures with Implanted LSI Sensors	12	confirmed	Mr. Nitish Rajoria	Keio University	Japan
4	A NEW CONCEPT IN VIRTUAL SIMULATION OF A SPACE STRUCTURE VIBRATION TEST	12'	no-show	Mr. Vincenzo Di Pietro	Thales Alenia Space Italia (TAS-I)	Italy
5	Design Strategy, Numerical Analysis and Testing of a Modular Satellite Structure	12	confirmed	Mr. Thomas A. Schervan	RWTH Aachen University	Germany
6	ESTCube-2 structure development, analysis, testing and verification	12	confirmed	Mr. Iaroslav Iakubivskyi	University of Tartu	Estonia
7	optimization for structure system of micro-satellite	12'	no-show	Mr. Liming Fan	School of Astronautics, Beihang University, Beijing 100191, PR China	China
8	formosat-5 satellite structure development and dynamic launch environment verification	12	confirmed	Mr. Jen-Chueh KUO	National Space Organization	Taiwan, China
9	Research on column buckling under internal pressure of plane-cone shaped metal bellows	12	confirmed	Mr. Muye Chen	Beijing institute of Astronautical Systems Engineering, Beijing	China
10	Multidisciplinary Design Optimization of a Satellite Structure by Additive Manufacturing	12	confirmed	Mr. Marius Bierdel	Fraunhofer EMI	Germany
11	On-ground testing of a restraint layer for inflatable modules for lunar orbital application	12	confirmed	Dr. Anton Kolozeznyy	TSNIIMASH	Russian Federation
12	A study on the Design and structural analysis of filament wound Composite Motor case with Inter metallic segment joint	12	confirmed	Mr. Paul Murugan J	Indian Space Research Organization (ISRO)	India
13	Verification of Diaphragm Analysis	12	confirmed	Mr. Stefan Weiland	MT Aerospace AG	Germany

session 1

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