Magneto Plasma Dynamic Thruster Using Water Propellant

Author:

MATSUURA Yusuke1,YANO Yasuyuki2,KAKAMI Akira3

Affiliation:

1. Department of Engineering, University of Miyazaki

2. Faculty of Engineering, University of Miyazaki

3. Department of Aeronautics and Astronautics, Tokyo Metropolitan University

Publisher

Japan Society for Aeronautical and Space Sciences

Reference8 articles.

1. 1) Nishiyama, K. and Kinefuchi, K.: 2. Current Status and Prospects of Electric Rocket Propulsion Technology, J. of Plasma and Fusion Research, 94-2 (2018), pp.60–65 (in Japanese).

2. 2) Stechman, C., and Harper, S.: Performance Improvements in Small Earth Storable Rocket Engines- An Era of Approaching the Theoretical, AIAA Paper 2010-6884, 2010.

3. 3) Casaregola, C.: Electric Propulsion for Station Keeping and Electric Orbit Raising on Eutelsat Platforms, Proceeding of 34th International Electric Propulsion Conference, Hyogo, Japan, IEPC-2015-97, 2015.

4. 4) Poole, M. and Monte, H.: Boeing Low-Thrust Geosynchronous Transfer Mission Experience, Proceeding of the 20th International Symposium on Space Flight Dynamics, Annapolis, USA, 2007.

5. 5) Tajmar, M. and C. de Matos: Water-arc Explosions as a Concept for Advanced Propulsion Thrusters, AIAA Paper 2000-3762, 2000.

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