TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN
Online ISSN : 1884-0485
ISSN-L : 1884-0485
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Magneto Plasma Dynamic Thruster Using Water Propellant
Yusuke MATSUURAYasuyuki YANOAkira KAKAMI
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2021 年 19 巻 4 号 p. 523-528

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This paper describes the design and performance of 100 kW class Magneto Plasma Dynamics Thruster (MPDT) using water as a liquid propellant. In general, MPDTs have a large thrust-to-power ratio and high specific impulse among the electric propulsion devices and use ammonium and hydrogen as a propellant. However, hydrogen propellant requires a high-pressure tank and damages materials, and ammonium is reactive and toxic. Hence, we propose to use water as an MPDT propellant, focusing on the storability and non-toxicity. The use of water propellant will simplify the propulsion systems and reduce size and weight because water necessitates no cryogenic devices nor chemically resistant materials. A 100-kW class prototype was designed to show that water MPDT yielded 1-kA class discharge current, which is necessary for thrust production in self-magnetic field types.

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© 2021 The Japan Society for Aeronautical and Space Sciences
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