Experimental Demo for Small Scale MHD Plasma Accelerator
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概要
- 論文の詳細を見る
The objective of the current MHD acceleration study is to thoroughly explain the compact experimental demo of MHD accelerator and to clarify some significant plasma variables both within and at the exit of the newly introduced mullite ceramic compact channel. The significant challenge of the current study is to use the 0.4-tesla neodymium magnetic as an MHD source, while the model rocket engine (C6-0, ESTES) is introduced and employed as a gas (plasma) source. The results of present demonstrations reveal that the highest gas velocity was calculated at 117.2 m/s using the gas pressure measurement through the pitot tube. The TOF method using two photo diodes showed the slowest speed of 50 m/s.
著者
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KIKUCHI Takashi
Nagaoka University of Technology
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SASAKI Toru
Nagaoka University of Technology
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KUBO Atsushi
Nagaoka University of Technology
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Harada Nobuhiro
Nagaoka Univ. Of Technol.
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RUNGSETTHAPHAT Vorathit
University of the Thai Chamber of Commerce, 126/1 Vibhavadee-Rungsit, Dindaeng 10400, Thailand
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RUNGSIRATHANA Thanat
University of the Thai Chamber of Commerce, 126/1 Vibhavadee-Rungsit, Dindaeng 10400, Thailand
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NAMPROM Anucha
University of the Thai Chamber of Commerce, 126/1 Vibhavadee-Rungsit, Dindaeng 10400, Thailand
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WIBOONPOL Theerawit
University of the Thai Chamber of Commerce, 126/1 Vibhavadee-Rungsit, Dindaeng 10400, Thailand
関連論文
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- Quantitative analysis on thin metal wire annealing at atmospheric plasma in cylindrical reactor
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- Velocity measurement and examination of the electrode shape in Pulsed MHD acceleration
- Study on Pulsed Linear MHD Accelerator using Model Rocket Engine
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