IAF Digital Library

4

session 4

Title: Electric Propulsion
type: oral
Description: This session is dedicated to all aspects of electric propulsion technologies, systems and applications.
Date: 2016-09-28
Time: 14:45
Room: Zapopan

IPC members

Co-Chair: Prof. Garri A. Popov, Research Institute of Applied Mechanics and Electrodynamics (RIAME), MAI, Russian Federation;
Co-Chair: Dr. Vanessa Vial, SAFRAN, France;
Rapporteur: Mr. Norbert Puettmann, Deutsches Zentrum für Luft- und Raumfahrt e.V. (DLR), Germany;

papers
Order	Time	Paper title	Mode	Presentation status	Speaker	Affiliation	Country
1		KEYNOTE: Beamed Energy Propulsion for future space launchers	30'	confirmed	Prof. Kimiya Komurasaki	University of Tokyo	Japan
2		Electrical Propulsion Application in China	15'	confirmed	Mr. Min Wang	China Academy of Space Technology (CAST)	China
3		ELECTRIC PROPULSION IN GERMANY: STATUS OF THE HEMP SYSTEM DEVELOPMENT, PRELIMINARY RESULTS OF THE LIFETIME TEST	15'	confirmed	Mr. Norbert Püttmann	DLR, German Aerospace Center	Germany
4		Electric Propulsion activities in Airbus DS 2016	15'	confirmed	Mrs. Nicoletta Wagner	Airbus DS GmbH	Germany
5		Application of pyrolytic graphite grids for a 20 mN ion thruster	15'	confirmed	Mr. Yoshiki Matsunaga	Japan Aerospace Exploration Agency (JAXA)	Japan
6		Development of a 10kW prototype ion thruster	15'	confirmed	Mr. yide zhao	Lanzhou Institute of Physics, China Academy of Space technology	China
7		Micro-propulsion based on vacuum arcs: Accessible technologies for CubeSat missions	15'	confirmed	Mr. Jonathan Kolbeck	George Washington University	United States
8		PPS®1350-E development status	15'	confirmed	Dr. Vanessa Vial	Snecma	France
9		effect of magnetic field configuration and anode configuration on 5 kw class anode layer type hall thruster	15'	confirmed	Mr. Yusuke Egawa	Kyushu University	Japan
10		Experimental research of radio-frequency ion thruster	15'	confirmed	Mr. Ruslan Akhmetzhanov	Research Institute of Applied Mechanics and Electrodynamics (RIAME), MAI	Russian Federation
11		Resistojet design for solid iodine propellant	15'	confirmed	Mr. Mario Angel Andrade Gonzalez		Mexico
12		Discharge and physical characteristics of an ablative liquid-fed pulsed plasma thruster for small satellites	15'	withdrawn	Dr. William Yeong Liang Ling	University of Tokyo	Japan
13		DEVELOPMENT OF A HARDWARE-IN-THE-LOOP TEST FACILITY USED FOR CHARACTERIZING THE NEW PULSED PLASMA THRUSTER PETRUS	15'	confirmed	Mr. Christoph Montag	Institute of Space Systems, University of Stuttgart	Germany
14		Operating the alternative propellant iodine in radio frequency ion thrusters	15'	withdrawn	Ms. Nina Sarah Mühlich	Justus-Liebig Universität Giessen	Germany