2006•VacuumRequires access

Performance test of micro ion thruster using microwave discharge

Yoshiyuki Takao, Hiroshi Kataharada, Takashi Miyamoto, Hirokazu Masui, Naoji Yamamoto, Hideki Nakashima

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Key concepts: Specific impulse, Ion thruster, Propellant, Geostationary orbit, Aerospace engineering, Microwave, Thrust, Electrically powered spacecraft propulsion

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Performance test of micro ion thruster using microwave discharge — Research Paper | ScholarLens