TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN
Online ISSN : 1884-0485
ISSN-L : 1884-0485
b) Electric and Advanced Propulsion
Development of a Laser-Electrostatic Hybrid Acceleration Propulsion System
Tatsuro SAKAIAkihiro OSAMURAHideyuki HORISAWA
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2014 年 12 巻 ists29 号 p. Tb_43-Tb_46

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The speed and number of ions in a laser-electrostatic hybrid thruster were experimentally estimated using a Faraday cup for various electrode configurations to determine the optimum electrode geometry. The results showed that, for a 10-mm-diameter electrode placed in front of a laser ablation target, the speed of ions increased with target voltages. The ion speeds, measured 80 mm away from the target, were 16 km/s and 32 km/s for target voltages of 0 V and 500 V, respectively, for a target–electrode gap of 20 mm.
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© 2014 The Japan Society for Aeronautical and Space Sciences
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