2021•Acta AstronauticaRequires access

Design and demonstration of a micro air-fed magnetoplasmadynamic thruster for small satellites

Zihao Wang, Youngho Eun, Xiaofeng Wu

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Key concepts: Specific impulse, Propellant, Thrust, Aerospace engineering, Electrically powered spacecraft propulsion, Propulsion, Ion thruster, Impulse (physics)

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Design and demonstration of a micro air-fed magnetoplasmadynamic thruster for small satellites — Research Paper | ScholarLens