2023
DOI: 10.1007/s44205-023-00046-x
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ECRA thruster advances: 30W and 200W prototypes latest performances

Abstract: The H2020 MINOTOR project focused on the study and the optimization of the ECRA thruster, an electric propulsion system for satellites. First, a 30 W prototype of this Electron Cyclotron Resonance Thruster (ECRT) is optimized. Then, a 200 W prototype is design based on these findings. The performances of both prototypes were assessed at two different facilities: at ONERA in France and at Justus Liebig University in Germany. Significant improvement of performances of both thrusters with the decrease of backgrou… Show more

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Cited by 11 publications
(4 citation statements)
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“…In this work, the absorbed microwave power (at frequency 2.45 GHz) is around 30 W. The thruster is fed with xenon at 1 and 2 SCCM flowrates. More details about the ECR thruster can be found in [12,[30][31][32][33][34].…”
Section: Results Inside the Ecr Thruster Plumementioning
confidence: 99%
“…In this work, the absorbed microwave power (at frequency 2.45 GHz) is around 30 W. The thruster is fed with xenon at 1 and 2 SCCM flowrates. More details about the ECR thruster can be found in [12,[30][31][32][33][34].…”
Section: Results Inside the Ecr Thruster Plumementioning
confidence: 99%
“…The electron cyclotron resonance thruster (ECRT) [3][4][5][6][7][8] is a type of electrodeless plasma thruster that relies on said resonance to couple electromagnetic power to the plasma electrons. In general, these devices consist of a cylindrical source immersed in a static, quasi-axial magnetic field.…”
Section: Introductionmentioning
confidence: 99%
“…The first method consists of MW injected in the TE 11 (transverse electric) mode from a cylindrical waveguide through a dielectric window; the second method instead brings MW power through a coaxial cable and relies on the presence of an additional central conductor to obtain a TEM propagation mode. The coaxial ECRT was first developed at ONERA (France), showing promising and competitive performance, [5][6][7][8] and raising interest in it elsewhere. 15,16 This design, however, is not strictly electrodeless and suffers the erosion of the central conductor and metallic deposition on the thruster backplate, 7 posing a limitation on lifetime.…”
Section: Introductionmentioning
confidence: 99%
“…In all instances, an applied magnetic field B a enables the propagation and absorption (resonant or not) of R waves in the plasma, reduces the plasma flux to the lateral walls, and conforms an external magnetic nozzle (MN) where the plasma is accelerated, producing magnetic thrust [12][13][14][15]. Currently, HPTs and ECRTs are still under development, and laboratory-demonstrated thrust efficiencies are still below 15%, with few exceptions [10,16,17].…”
mentioning
confidence: 99%