IAF Digital Library

6A

session 6A

Title: Generic Technologies for Small/Micro Platforms
Description: This session covers emerging and promising generic technologies for small and micro platforms. Real-life examples are particularly encouraged, both recently launched and shortly to be launched (next 3 years).
Date: 2017-09-28
Time: 09:45
Room: Panorama Room 1

IPC members

Co-Chair: Mr. Philip Davies, Surrey Satellite Technology Ltd (SSTL), United Kingdom;
Co-Chair: Dr. Jian Guo, Delft University of Technology (TU Delft), The Netherlands;

papers
Order	Time	Paper title	Mode	Presentation status	Speaker	Affiliation	Country
1		ALL-ELECTRIC MINI-PLATFORM AND VERY-LEO HI-RES CONSTELLATION	15	confirmed	Mr. Vincenzo Stanzione	Sitael Spa	Italy
2		Application of Plug-and-Play Integrated Micro-Propulsion System for Micro-Satellite Based on Additive Material Manufacturing	15	no-show	Mrs. Liu Yiwei		China
3		Integrating a large nanosatellite from CubeSat components – Challenges and solutions	15	confirmed	Mr. Clemens Horch	Fraunhofer EMI	Germany
4		A low cost self-powered wireless attitude sensor for CubeSats	15	confirmed
5		The development of a passive de-orbit subsystem for small and micro satellites	15	confirmed	Dr. Thomas Sinn	HPS GmbH	Germany
6		Improved Attitude Determination for TUBiX20: Evaluation, Integration and Testing of a Fluxgate Magnetometer	15	withdrawn	Mr. Marc Lehmann	Technische Universität Berlin	Germany
7		a newly androgynous design of soft docking mechanism for micro/small satellites	15	no-show	Dr. Xiang Zhang	College of Aerospace Science and Engineering, National University of Defense Technology	China
8		Fault Detection Isolation and Recovery Approach for PROBA-3 RVX Experiment	15	withdrawn	Ms. Silvana Radu	Institute of Space Science	Romania
9		A Redundant and Integrated Avionics for 12U CubeSat	15	confirmed	Dr. Guanghui Liu	Northwestern Polytechnical University	China
10		Micro- and Nano- Re-entry Spacecraft Technology Developments	15	confirmed	Dr. Sean Tuttle	UNSW Australia	Australia
11		on-ground verification of attitude control system for 50-kg-class microsatellites using a hardware-in-the-loop-simulator	15	confirmed	Mr. Shinya Fujita	Tohoku University	Japan
12		Scalability and Modularity as Dimensions of Flexibility of a Microsatellite Platform	15	confirmed	Dr. Frank Dannemann	German Aerospace Center (DLR)	Germany