session 2

Title: Space Structures II - Development and Verification (Deployable and Dimensionally Stable Structures)
Description: The topics to be addressed include evaluation of analysis versus test results for deployable and dimensionally stable structures, e.g. reflectors, telescopes, antennas; examination of both on-ground and in-orbit testing, thermal distortion and shape control, structural design, development and verification; lessons learned.
Date: 2015-10-13
Time: 09:45
Room: Oranim 1 (ICC, lower level)

IPC members

Co-Chair: Prof. Paolo Gasbarri, University of Rome “La Sapienza”, Italy;
Co-Chair: Mr. Jean-Alain Massoni, Thales Alenia Space France, France;
Rapporteur: Prof. Pierre Rochus, CSL (Centre Spatial de Liège), Belgium;

papers
Order	Paper title	Mode	Presentation status	Speaker	Affiliation	Country
1	design and analysis of a composite sandwich solar array structure for the eu:cropis compact satellite with as few release mechanisms as possible	12'	confirmed	Mr. Thilo Glaser	German Aerospace Center (DLR)	Germany
2	Development of calculation model of large-size thermo-dimensionally stable structure of composite materials	12'	confirmed	Mr. Serhii Kushnirenko	Yuzhnoye State Design Office	Ukraine
3	Development of Elastic Forces Model for High Area-to-Mass Ratio Flexible Spacecraft	12'	withdrawn	Mr. Dayu ZHANG	National Key Laboratory of Aerospace Flight Dynamics,Northwestern Polytechnical University,Xi'an,	China
4	Environmental Testing and Analysis of a Boom Deployment Mechanism for GOSSAMER-2	12'	confirmed	Mr. Sebastian Meyer	German Aerospace Center (DLR)	Germany
5	Deployment and Post Grasping Issues for a Light Weight Robotic Arm Mounted on a Small Space-Services	12'	confirmed	Prof. Paolo Gasbarri	Università di Roma "La Sapienza"	Italy
6	mechanical characterization of deployable thin shell cfrp-booms for the cubeSat “de-orbit sail”	12'	confirmed	Mr. Martin Zander	German Aerospace Center (DLR)	Germany
7	AstroTube Max: The development and testing of a low mass extendible CFRP telescopic boom for satellite applications.	12'	confirmed	Mr. Vincent Fraux	Oxford Space Systems	United Kingdom
8	use of composite materials based on cyanate ester resins for manufacture of space qualified structures with high dimentional stability	12'	confirmed	Dr. Gabriel Sznejer	Rafael Advanced Defense Systems Ltd.	Israel
9	ground testing of a 8-meter 4-quadrant scalable solar sail	12'	confirmed	Dr. Xinghua Zhang	Qian Xuesen Laboratory of Space Technology	China
10	Thermal deformation on laser retro-reflectors of LARES satellite	12'	confirmed	Prof. Antonio Paolozzi	Sapienza University of Rome	Italy
11	Model and analysis of bi-hoop circular deployable truss	12'	withdrawn	Prof.Dr. Minger Wu	Tongji University	China

session 2

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