rootbrowseIAC-19C2session 22. Space Structures II - Development and Verification (Deployable and Dimensionally Stable Structures)Papers1. Compressive response and failure of a micromechanical model for confined unidirectional fiber reinforced composite2. 5.0 meter truncated solid shell reflector : ArianeGroup alternative to expensive deployable mesh reflectors3. Efficient Analysis of Geometrically Nonlinear Deployable Thin Shell Structures Using Carrera Unified Formulation4. Design Analysis of Cable-Actuated Cylindrical Tensegrity Booms5. a two-arm flexible space manipulator system for post-grasping manipulation operations of a passive target object6. Design, analysis and testing of a novel deployable telescope for earth observation using small satellites7. Evaluation of the effect of the compression stiffness and the bending stiffness on the deployment of a membrane-like spacecraft with the multi-particle method8. Experimental Verification of Two-Dimensional Self-Deployable Space Structures with Convex-Panel9. space demonstration of occulter using self-deployable membrane truss10. Development and Testing of an Antenna Deployment System for Nanosatellite Applications11. TriTruss: A New and Novel Structural Concept Enabling Modular Space Telescopes and Space Platforms12. An ultra-compact helical antenna for small satellites. Micromechanics based Reliability Analysis for Laminated Composite Structures. SCIENTIFIC PROBLEMS AND ENGINEER RESOLVENT DURING DEVELOPMENT OF LARGE DEPLOYABLE MESH ANTENNA. Thermal Distortion Compensation for Improving Electrical Performance of Space Reflector Antenna