Art

J-GLOBAL ID：201202229169898019   Reference number：12A1257381

Improvement of thrust performance in a Magneto-Plasma-Dynamic Thruster (MPDT) with externally applied magnetic field configuration

外部磁場形状によるMPDT推進性能の改善

Author (6)： WATANABE HIROSHI (東北大) ,  OKAWA KOHEI (東北大) ,  HASHIMA YUKO (東北大) ,  IZAWA YUKI (東北大) ,  TANAKA NOZOMI (東北大) ,  ANDO AKIRA (東北大)
Material： 電気学会プラズマ研究会資料  (電気学会研究会資料)
Volume： PST-12  Issue： 49-67  Page： 69-74  Publication year： Aug. 08, 2012 
JST Material Number： Z0951A  Document type： Proceedings
Article type： 原著論文  Country of issue： Japan (JPN)  Language： JAPANESE (JA)

Thesaurus term： *propulsion system ,  electric propulsion ,  magnetic field effect ,  shape effect ,  thrust ,  *propulsion efficiency ,  plasma flow ,  plasma diagnostics ,  plasma density ,  plasma temperature ,  electron density ,  propulsive performance ,  plasma device ,  Mach probe ,  *Magneto Plasma Dynamic thruster ,  position dependence ,  magnetic nozzle ,  *electrically powered spacecraft propulsion ,  *internal combustion engine ,  *heat engine
Semi thesaurus term： *electric rocket engine

JST classification (1)： Rocket engines  (PB02050J)

Reference (4)：

• (1) A. Sasoh "Generalized Hall acceleration", Journal of Propulsion and Power, Vol.10, No.2, pp.251-254 (1991)
• (2) A. W. Blackstock, D. B. Fradkin, K. W. Liewer, D. J. Roehling, T. F. Stratton, and M. Willams "Experiments using a 25-kW hollow cathode lithium vapor MPD arcjet", AIAA Journal Propulsion and Power, Vol.8, No.5, pp.886-894 (1970)
• (3) H. Tahara, F. Takiguchi, Y. Kagaya and T. Yoshikawa "PERFORMANCE CHARASTESTICS AND DISCHARGE FEATURES OF A QUASI-STEADY APPLIED-FILED MPD ARCJET", 22nd Int. Electric Propulsion Conf, Paper IEPC-91-073 (1991)
• (4) R. Yanagi and I. Kimura "New Type of Target for the Measurement of Impulse Bits of Pulsed Plasma Thrusters", Journal of Spacecraft and Rocket, Vol.19, No.3, pp.246-249 (1982)

Terms in the title (1)： 推進性能