Effect of Solute Mixing in the Liquid Propellant of a Pulsed Plasma Thruster
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概要
- 論文の詳細を見る
Sodium chloride or ammonia was dissolved in the water propellant of pulsed plasma thrusters to improve the performance. Pulsed plasma thrusters using liquid propellant utilize water as attractive alternative instead of Teflon. Water propellant enables the controlling propellant mass flow and leads high specific impulse. However, liquid propellant pulsed plasma thrusters have larger plasma resistance and lower thrust power ratio than common Teflon propellant thruster. Here, sodium chloride and ammonia solution of water was examined to decrease that plasma resistance. As a result, emission lines attributed from the solute were observed using sodium chloride aqueous solution propellant, and a 5 % reduction of the plasma resistance was shown, and the thrust to power was increased. However, ammonia aqueous solution decreased the thruster performance.
- Elsevierの論文
著者
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Arakawa Y
Department Of Aeronautics And Astronautics University Of Tokyo
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Koizumi Hiroyuki
Department Of Aeronautics And Astronautics University Of Tokyo
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Komurasaki K
Graduate School Of Engineering Tokyo University
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Arakawa Yoshihiro
Department Of Aeronautics And Astronautics University Of Tokyo
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