2021
DOI: 10.1088/1361-6463/ac4451
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Deflections of dynamic momentum flux and electron diamagnetic thrust in a magnetically steered rf plasma thruster

Abstract: Two-dimensional characterization of the plasma plume is experimentally performed downstream of a magnetically steered radiofrequency plasma thruster, where the ion beam current, the ion saturation current, and the horizontal dynamic momentum flux, are measured by using the retarding field energy analyzer, the Langmuir probe, and the momentum vector measurement instrument, respectively, in addition to the previously measured horizontal thrust. The measurements show the deflections of the dynamic momentum flux i… Show more

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Cited by 8 publications
(8 citation statements)
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“…The Gaussian deconvolution method, or Gaussian fitting, has been used to obtain the ion-energy distribution function from the I-V characteristics measured by a retarding field energy analyzer 2,16,19 . This involves an iterative process of integrating a Gaussian curve that models the ion-energy distribution function until the raw I-V data are reconstructed.…”
Section: Gaussian Deconvolutionmentioning
confidence: 99%
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“…The Gaussian deconvolution method, or Gaussian fitting, has been used to obtain the ion-energy distribution function from the I-V characteristics measured by a retarding field energy analyzer 2,16,19 . This involves an iterative process of integrating a Gaussian curve that models the ion-energy distribution function until the raw I-V data are reconstructed.…”
Section: Gaussian Deconvolutionmentioning
confidence: 99%
“…The ion-energy distribution function has usually been computed by obtaining the first derivative of the collected current over the discriminator voltage 2,5,6,[14][15][16][17][18][19] . It can be shown that, by assuming a one-dimensional velocity distribution 14 , the ion-energy distribution g i (ε i ) is proportional to the negative derivative of the collected current I C with respect to the discriminator grid voltage V D :…”
Section: Introductionmentioning
confidence: 99%
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“…The concept of thrust vectoring via a steerable magnetic nozzle has also been the subject of different research campaigns [27][28][29][30]. This could allow for a mechanically simpler and more reliable orbit and attitude control mechanism since it does not comprise any moving or rotating components.…”
Section: Introductionmentioning
confidence: 99%
“…the location of plasma excitation coincides with the magnetic nozzle throat), the experiments presented herein are conducted in an RF plasma device in which the antenna and the coils are not placed on the same axial location (see figure 3). Studies with a similar experimental design have been carried out by [16,21,29,[31][32][33][34]. In this configuration, the plasma is created remotely with respect to the magnetic nozzle throat.…”
Section: Introductionmentioning
confidence: 99%