400-V Bus-Direct Driven High-Power Arcjet Thruster Using Dimethyl Ether as Additive for Extending Lifetime

Author:

KISHIDA Toshihisa1,MURATA Hiroaki2,YANO Yasuyuki3,KAKAMI Akira1

Affiliation:

1. Department of Mechanical Design Systems Engineering, University of Miyazaki

2. Department of Mechanical Systems Engineering, University of Miyazaki

3. Technical Center, University of Miyazaki

Publisher

Japan Society for Aeronautical and Space Sciences

Reference7 articles.

1. 1) Kuriki, K. and Arakawa, Y.: Introduction to Electric Propulsion Rockets, University of Tokyo Press, Tokyo, 2003, pp. 7–11 (In Japanese).

2. 2) Jahn, R.G.: Physics of Electric Propulsion, Dover Publications, INC., New York, 1996, p. 126–133.

3. 3) Sutton, G.P. and Biblarz, O.: Rocket Propulsion Elements 7th edition, JOHN WILEY & SONS, INC., New York, 2001, pp. 636– 639.

4. 4) Stephenson, R. R.: Electric Propulsion Development And Application In The United States, Proceedings of International Electric Propulsion Conference, IEPC-95-01, Moscow, Russia, Sept. 1995.

5. 5) Nishida, M.: Arcjet thruster, Trans. JSME, 69(2003) pp. 3–9. (in Japanese).

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