rootbrowseIAC-23C2session 22. Space Structures II - Development and Verification (Deployable and Dimensionally Stable Structures)Papers1. Thermal stresses and buckling of variable stiffness composite laminates2. A higher-order beam finite element for the folding analysis of composite-made booms with silicone matrix and carbon fibers3. Analysis of out-of-plane thermal deformation of the ultralight phased array antenna4. Unfolding methods of a two orders of magnitude mechanical volume reduced spheroid Tumbleweed Mobile Impactor5. A Proposal for a Lightweight Deployable Large Membrane Dipole Array Antenna6. Non-Inertial Structural Effects in Flexible Spacecraft with Spinning Appendage7. Tensegritical model rocket fuselage based on prismatic unit cells structures for impact absorbing and energy distributing purposes.8. Preliminary Design of a CubeSat Demonstrator for an Origami-inspired Deployable Structure9. Relaxation effects due to the stowage phase on the deployment of ultra-thin composite booms10. Analysis of the angular motion dynamics of a prospective descent vehicle equipped with a deployable braking11. Degradation processes of Al/MgF2 UV telescope mirrors under high energy photons12. Additive Manufacturing With Molten Lunar Regolith Under Vacuum Conditions