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: 2017-09-26
Time: 09:45
Room: Panorama Room 2

IPC members

Co-Chair: Prof. Paolo Gasbarri, University of Rome “La Sapienza”, Italy;
Co-Chair: Dr. Oliver Kunz, Beyond Gravity, Switzerland;
Rapporteur: Prof. Pierre Rochus, CSL (Centre Spatial de Liège), Belgium;

papers
Order	Paper title	Mode	Presentation status	Speaker	Affiliation	Country
1	The effects of the center of mass motion on the relative translation and attitude motion of space tugs in close proximity of rendezvous and docking/berthing operations.	12	confirmed	Mr. Luciano Unfried	Aeronautic Institute of Technology (ITA)	Brazil
2	Towards a European Large Deployable Antenna: Overview of Current Development Activities	12	confirmed	Dr. Thomas Sinn	HPS GmbH	Germany
3	design, test and comparison of mechanical support principles to increase the robustness of deployable thin-shell cfrp-booms of the deorbiting device adeo	12	confirmed	Mr. Martin Zander	German Aerospace Center (DLR)	Germany
4	parametric analysis of a controlled deployable space manipulator used for capturing a non-cooperative satellite	12	confirmed	Mr. Angelo Stolfi	Università di Roma "La Sapienza"	Italy
5	High-Precision Positioning of Reflector Segment by Using Kinematic Couplings for Balloon-Borne Radio Telescope	12	confirmed	Dr. Hiroaki Tanaka	National Defense Academy	Japan
6	Decrement Properties of Deployment Torque for Self-deployable Tubular CFRP Booms under Stored State	12	confirmed	Mr. Takaomi Chubachi	Tokyo Institute of Technology	Japan
7	toward a multifunctional interface for future planetary and orbital missions	12	confirmed	Dr. ROBERTO PALAZZETTI	University of Strathclyde	United Kingdom
8	Design and analysis of bistable composite booms	12	withdrawn	Ms. Orzuri Rique	Purdue University	United States
9	A Design Method to Keep Asymmetrical Ring Truss Reflector Surface Stable and Test Verification	12	confirmed	Mr. Hui Wang		China
10	Thermo-structural analysis during ascent flight and atmospheric reentry for SARA capsule	12	withdrawn	Dr. ELCIO JERONIMO DE OLIVEIRA	Institute of Aeronautics and Space (IAE)	Brazil
11	Improvement of Sail Storage Structure and Deployment Mechanism for Next Spin-type Solar Power Sail-craft	12	confirmed	Dr. Osamu Mori	Japan Aerospace Exploration Agency (JAXA)	Japan
12	Static and dynamic analysis of partially wrinkled membranes for tethered spinning solar sail applications	12	confirmed	Dr. Chao Xu	Northwestern Polytechnical University	China
13	Passive Nonlinear Actuators for Deploying the Mesh Antennas	12	confirmed	Dr. Zhihua Zhao	Tsinghua University	China
–	Highly Compressible Origami Bellows for Microgravity Drilling-Debris Containment		withdrawn	Mr. Jared Butler	Brigham Young University	United States
*	Design and Experiment for A High Precision Reflector		withdrawn	Dr. XiaoFei Ma	Xi’an Institute of Space Radio Technology	China

session 2

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