rootbrowseIAC-15C2session 22. Space Structures II - Development and Verification (Deployable and Dimensionally Stable Structures)Papers1. design and analysis of a composite sandwich solar array structure for the eu:cropis compact satellite with as few release mechanisms as possible2. Development of calculation model of large-size thermo-dimensionally stable structure of composite materials3. Development of Elastic Forces Model for High Area-to-Mass Ratio Flexible Spacecraft4. Environmental Testing and Analysis of a Boom Deployment Mechanism for GOSSAMER-25. Deployment and Post Grasping Issues for a Light Weight Robotic Arm Mounted on a Small Space-Services6. mechanical characterization of deployable thin shell cfrp-booms for the cubeSat “de-orbit sail”7. AstroTube Max: The development and testing of a low mass extendible CFRP telescopic boom for satellite applications.8. use of composite materials based on cyanate ester resins for manufacture of space qualified structures with high dimentional stability9. ground testing of a 8-meter 4-quadrant scalable solar sail10. Thermal deformation on laser retro-reflectors of LARES satellite11. Model and analysis of bi-hoop circular deployable truss