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: 2023-10-03
Time: 10:15
Room: BCC A1

IPC members

Co-Chair: Prof. Paolo Gasbarri, University of Rome “La Sapienza”, Italy;
Co-Chair: Dr. David E. Glass, National Aeronautics and Space Administration (NASA), United States;

papers
Order	Time	Paper title	Mode	Presentation status	Speaker	Affiliation	Country
1	10:15	Thermal stresses and buckling of variable stiffness composite laminates	12	confirmed	Ms. Rebecca Masia	Politecnico di Torino	Italy
2	10:27	A higher-order beam finite element for the folding analysis of composite-made booms with silicone matrix and carbon fibers	12	confirmed	Prof. Alfonso Pagani	Associazione Italiana di Aeronautica e Astronautica (AIDAA)	Italy
3	10:39	Analysis of out-of-plane thermal deformation of the ultralight phased array antenna	12	confirmed	Dr. Ryo Higuchi	University of Tokyo	Japan
4	10:51	Unfolding methods of a two orders of magnitude mechanical volume reduced spheroid Tumbleweed Mobile Impactor	12	confirmed	Mr. Nils Neumeister	Team Tumbleweed	Austria
5	11:03	A Proposal for a Lightweight Deployable Large Membrane Dipole Array Antenna	12	confirmed	Mr. Ryohei Orii	The Graduate Universty for Advanced Studies[SOKENDAI]	Japan
6	11:15	Non-Inertial Structural Effects in Flexible Spacecraft with Spinning Appendage	12	confirmed	Mr. David Paolo Madonna	Sapienza University of Rome	Italy
7	11:27	Tensegritical model rocket fuselage based on prismatic unit cells structures for impact absorbing and energy distributing purposes.	12	confirmed	Mr. Bryan Méndez Medina	Universidad de Costa Rica	Costa Rica
8	11:39	Preliminary Design of a CubeSat Demonstrator for an Origami-inspired Deployable Structure	12	confirmed	Ms. Joshika Sachithanandan	Delft University of Technology (TU Delft), The Netherlands	The Netherlands
9	11:51	Relaxation effects due to the stowage phase on the deployment of ultra-thin composite booms	12	confirmed	Mr. Daniele Tortorici	Sapienza University of Rome	Italy
10	12:03	Analysis of the angular motion dynamics of a prospective descent vehicle equipped with a deployable braking	12	confirmed	Mr. Andrey Kukharenko	Bauman Moscow State Technical University	Russian Federation
11	12:15	Degradation processes of Al/MgF2 UV telescope mirrors under high energy photons	12	confirmed	Ms. Daria Pasynkova	Bauman Moscow State Technical University	Russian Federation
12	12:27	Additive Manufacturing With Molten Lunar Regolith Under Vacuum Conditions	12	confirmed	Mr. Simon Stapperfend	TU Berlin	Germany

session 2

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