session 2

Title: Enabling Technologies for Space Systems
type: oral
Description: This session will focus on innovative, technological developments that are usually high risk, but which have the potential to significantly enhance the performance of existing and new space systems. Enabling innovative technologies for space applications often result from spin-ins which will be discussed during the session, together with potential spin-offs. Examples include instrumentation, biotechnology, components, micro- and nano-technology, MEMs, advanced new structures and software techniques.
Date: 2016-09-27
Time: 14:45
Room: Salon de Eventos 5

IPC members

Co-Chair: Mr. Xavier Roser, Thales Alenia Space France, France;
Co-Chair: Mr. Steven Arnold, The John Hopkins University Applied Physics Laboratory, United States;
Rapporteur: Mr. Eiichi Tomita, Japan Aerospace Exploration Agency (JAXA), Japan;

papers
Order	Paper title	Mode	Presentation status	Speaker	Affiliation	Country
1	Automated Design of CubeSats and Small Spacecrafts	15'	confirmed	Prof. Jekanthan Thangavelautham	Arizona State University	United States
2	Developing a plug and play solution for satellite manufacturing	15'	confirmed	Mr. Ran Qedar	Space Products and Innovation	Germany
3	On the Development of a Novel CubeSat Standard Structure for Modern Missions	15'	withdrawn	Mr. Craig Clark	Clyde Space Ltd.	United Kingdom
4	An Versatile Approach for Assembling Reflectors in Space	15'	withdrawn	Dr. Ling-bin ZENG	Shanghai Aerospace System Engineering Institute	China
5	Self-supervised learning as an enabling technology for future space exploration robots: ISS experiments	15'	confirmed	Dr. Guido de Croon	TU Delft	The Netherlands
6	STARARM: Personal Robotic Arm	15'	confirmed	Mr. Chrishma Singh-Derewa	National Aeronautics and Space Administration (NASA), Jet Propulsion Laboratory	United States
7	capabilities of stereo vision systems for future space missions	15'	confirmed	Mr. Marco Carpentiero	Sapienza University of Rome	Italy
8	Space Multi-Rigid Arm System based Space Flexible Capture Arm Model Constraints Design	15'	no-show	Dr. Fan Yang	Academy of Equipment	China
9	Rapid Thermal Deformation Analysis of On-orbit Satellites Based on Telemetric Data of Temperature	15'	confirmed	Dr. Yechi Zhang	Institute of Spacecraft System Engineering,China Academy of Space Technology (CAST)	China
10	Spacecraft joining using a tethered electromagnetic probe	15'	confirmed	Mr. Matteo Duzzi	CISAS – “G. Colombo” Center of Studies and Activities for Space, University of Padova	Italy
11	Modeling and performance analysis of a new inflatable electrodynamic tether for satellite deorbiting	15'	confirmed	Mr. Wei Zheng	China Academy of Space Technology (CAST)	China
12	Dron Simulation for the Control of a Satellite Trajectory with fixed attitude	15'	confirmed	Mr. Raziel Campos-Sanchez	INAOE	Mexico
–	Verification of Space Flexible Capture Mechanism and its Multi-body Dynamics by On-orbit Test			Prof. Zhenghong Dong	Academy of Equipment	China

session 2

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