2018•CEAS Space JournalRequires access

Finite element modelling and performance optimization of an ion thruster depending on the nature of the propellant

Ionuț Florian Popa, Anna-Maria Theodora Andreescu, Dan Ifrim, Radu Mihalache, Dragoș Mihai, Grigore Cican

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Key concepts: Propellant, Specific impulse, Ion thruster, Propulsion, Spacecraft propulsion, Aerospace engineering, Electrically powered spacecraft propulsion, Xenon

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Finite element modelling and performance optimization of an ion thruster depending on the nature of the propellant — Research Paper | ScholarLens