2022
DOI: 10.1007/s44205-022-00034-7
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Experimental characterization of thrust production mechanisms in a magnetic nozzle ECR thruster

Abstract: Direct thrust measurements have been performed on a low-power (30 W) ECR plasma thruster operated with xenon. The total thrust, the force exerted on the walls of the source (thermal thrust), and the force exerted on the permanent magnet (magnetic thrust) have been measured separately for various operating conditions (power and flowrate). The results are compared for two magnetic field topologies (with a different magnetic field gradient and divergence). The magnetic thrust dominates thermal thrust for most ope… Show more

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Cited by 2 publications
(3 citation statements)
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“…Data interpretation can be challenging due (mainly) to a high-energy ion beam [12]. On the other hand, CP measurements have already given access successfully to electron density profiles in the near field of the thruster [11,35].…”
Section: Results Inside the Ecr Thruster Plumementioning
confidence: 99%
“…Data interpretation can be challenging due (mainly) to a high-energy ion beam [12]. On the other hand, CP measurements have already given access successfully to electron density profiles in the near field of the thruster [11,35].…”
Section: Results Inside the Ecr Thruster Plumementioning
confidence: 99%
“…The magnetic nozzle (MN) is a device used for providing constraint to plasma and converting the internal energy of plasma into kinetic energy. It is commonly used in electric propulsion, especially with neutralizer-free thrusters [1,2], such as helicon plasma sources [3][4][5][6], electron-cyclotron-resonance sources [7][8][9][10], Magnetoplasmadynamic thrusters [11], or vacuum cathode arc thrusters [12].…”
Section: Introductionmentioning
confidence: 99%
“…Introducing equations (5) and (6) to equation(10) leads to a simplified equation shown in equation (11):…”
mentioning
confidence: 99%