REVIEW 2 major objections 6 minor 51 references
Lower-Hybrid Drift Instabilities in a magnetic nozzle
T0 review · 2 major / 6 minor · reviewed 2026-08-11 · deepseek-v4-flash
Pith's one-line read Parallel gradients can drive magnetic-nozzle instabilities even at zero axial wavenumber.
desk verdict A serious fluid-theory advance for E×B instabilities that adds parallel gradients to the dispersion relation; the central claim is credible but rests on one modeling assumption that needs a kinetic benchmark. read the letter →
The pith
A machine-rendered reading of the paper's core claim, the machinery that carries it, and where it could break.
The reading
What carries the argument
The load-bearing object is the low-frequency dispersion relation, Eq. (III.30), obtained by closing the linearized two-fluid equations with quasineutrality. It uses the electron Doppler-shifted frequency ωe and the gyroviscously corrected frequencies ω⊥ and ω∥ from Eqs. (III.1)–(III.2), with parallel-gradient coupling entering through Ω∥ (Eq. (III.25)) and σ∥ (Eq. (III.26)). A key step is selecting the wave-amplitude envelope along the magnetic field, Eq. (III.24), ∇∥ ln(n0φ1/B) = (1/2)∇∥ ln(pe0/B) in the long-wavelength limit, so that the collisionless dispersion relation remains real; Appendix B justifies this choice with a 1D WKB argument. The generalized instability criterion, Eq. (IV.7), then shows how the interspecies drift, perpendicular gradient drifts, and parallel-gradient or parallel-propagation terms combine, and the quasi-linear flux, Eq. (VI.8), has the sign of kθ and is directed against the perpendicular gradient of n0/B².
What would settle it
A local kinetic (Vlasov) linear stability calculation at point B of Table V.1, with k∥ = 0 and the same equilibrium gradients, would settle the central claim: if it finds no growing lower-hybrid mode where the modified Simon–Hoh criterion predicts stability, the parallel-gradient mechanism is an artifact of the fluid closure or the amplitude-envelope assumption; if it finds one, the claim is supported.
Extended reading notes
Core claim
The central discovery is that the low-frequency dispersion relation, Eq. (III.30), which includes parallel equilibrium gradients, magnetic curvature, finite Larmor radius, collisions, gyroviscosity, and 3D wave propagation, generalizes earlier fluid dispersion relations for E×B plasmas. Within this relation, the parallel gradient terms enter through the frequencies Ω∥ and σ∥, and they open a destabilization channel: even when the perpendicular gradient condition for the modified Simon–Hoh instability fails, and even with k∥ = 0, the parallel gradients of n0, B, and Te can drive a lower-hybrid drift instability. The paper states this directly: parallel inhomogeneities 'may drive instabilities even in the absence of axial propagation.' This result implies that no local fluid stability analysis of a magnetic nozzle is complete without retaining the parallel gradients of equilibrium plasma quantities.
Load-bearing premise
The derivation fixes the spatial shape of the wave's amplitude along the magnetic field ahead of time, so that the collisionless dispersion relation stays real; if the true amplitude envelope differs from this WKB-consistent choice, the stability criteria derived could change.
Editorial extensions
If this is right
- No local fluid stability analysis of an axisymmetric E×B discharge in a magnetic nozzle is complete unless it retains parallel gradients of equilibrium quantities; analyses restricted to perpendicular gradients can miss unstable regions.
- Magnetic nozzles are predicted to host essentially azimuthal lower-hybrid drift instabilities at 1 kHz–1 MHz across wide regions of the plume, including regions where the modified Simon–Hoh condition is not satisfied, offering a candidate explanation for observed fluctuations.
- Finite parallel propagation k∥ can stabilize some perpendicular-gradient-driven modes in the near plume, but it can also create short-wavelength onset regions in the far plume where perpendicular gradients are weak.
- The quasi-linear cross-field electron transport is directed against the perpendicular gradient of n0/B², so the instability acts to relax the density and profile gradients that produced the drift, making the growth self-limiting.
- Collisions are secondary for the most unstable drift-gradient modes over the explored parameter range, but they can extend instability into regions where gradient drives are weak and slightly reduce peak gradient-driven growth rates.
Reading between the lines
- If confirmed experimentally with azimuthal mode-resolved measurements, the predicted 1 kHz–1 MHz instability band could serve as a non-intrusive local probe of gradient steepness in the nozzle plume.
- The same parallel-gradient mechanism should operate in other E×B devices with field-aligned gradients, such as Hall thruster plumes and mirror-like divergent magnetic fields, so the local model could be tested against global simulations that resolve k∥.
- The amplitude-envelope condition, Eq. (III.24), is a testable prediction: a fully self-consistent linearized solution that solves for the envelope of φ1 along the field should reproduce this shape at long wavelength if the mechanism is real.
- The quasi-linear transport result, being outward for radially decreasing density, aligns with observations of wave-driven outward electron flux and implies that instabilities may reduce magnetic nozzle efficiency by flattening the density gradient rather than acting as a simple anomalous diffusion.
Editorial analysis
A structured set of objections, weighed in public.
Referee Report
Summary. This paper derives a local, linear, electrostatic dispersion relation for low-frequency instabilities in a partially magnetized E×B plasma, retaining two-dimensional equilibrium gradients (perpendicular and parallel to the magnetic field), magnetic curvature, finite Larmor radius effects, gyroviscosity, collisions, and three-dimensional wave propagation. The model is applied to equilibrium profiles from hybrid simulations of a helicon-thruster magnetic nozzle, yielding instability criteria and 2D maps of maximum growth rate, frequency, and wavenumber. The paper reports predominantly azimuthal instabilities in the 1 kHz–1 MHz range, including cases where parallel equilibrium gradients destabilize modes with k∥=0, and a quasi-linear analysis indicating cross-field electron transport that opposes the equilibrium gradient of n0/B^2.
Significance. If the central claim holds, the paper generalizes the standard fluid dispersion relations for E×B plasmas (MSHI, MTSI) to include parallel equilibrium gradients, with the substantive prediction that no local fluid stability analysis of a magnetic nozzle is complete without these terms. The derivation is analytically explicit, recovers known limits in Eqs. (III.31)–(III.33), and provides simple instability criteria (IV.7) that can be tested in other devices. The application to a publicly available simulation dataset and the falsifiable quasi-linear transport prediction are additional strengths. However, the load-bearing envelope-shape assumption in Eq. (III.24) is not yet derived from the linearized initial-value problem, and the quantitative maps include growth-rate maxima outside the stated kρe<1 fluid validity. These issues do not necessarily invalidate the approach, but they currently limit confidence in the headline predictions.
major comments (2)
- [Section III, Eq. (III.24); Appendix B] The dispersion relation's dependence on parallel equilibrium gradients, and the derived stability criteria, rest on an imposed envelope shape. In Section III, Eq. (III.24) sets ∇∥ ln(n0φ1/B) = (1/2)∇∥ ln(pe0/B) − k^2ρe^2 ∇∥ ln Te specifically to force Im{Ω∥²}=0. This choice is presented as necessary to avoid spurious energy sources, and Appendix B justifies it by analogy to a 1D scalar WKB wave equation (B.1)–(B.10). However, the linearized electron system (II.6)–(II.9) is a coupled four-field system; the amplitude of φ1 (or of n0φ1/B) is fixed by the transport equation of the full system, not by requiring the dispersion relation to be real. If the physical envelope differs from Eq. (III.24), the coefficients of Eq. (III.30) acquire imaginary parts and the reactive-instability criteria (IV.5)–(IV.7) no longer follow. In particular, the claim that parallel gradients alone destabilize modes at k∥=0 (points B and C in Figs. V.3–V.5, and the abstract's statement) passes through this assumption. To establish the central claim, the authors need to derive the envelope shape from the linearized initial-value problem, or demonstrate that Eq. (III.24) is the unique choice that eliminates artificial sources/sinks in the full model, not merely in the scalar analogue of Appendix B.
- [Section V, Figs. V.3, V.4, V.5] The quantitative maps in Fig. V.5, and the representative dispersion relations in Figs. V.3 and V.4, present growth-rate maxima at kρe = O(1). The fluid model is stated to be valid only for kρe < 1 (Section II and the closing paragraph of Section V). The authors acknowledge that 'in those points where γmax is reached for k*ρe=1, a kinetic formulation of the problem would be more suitable,' but the 2D maps of γmax, ω*r, and k* are drawn using those maxima, and the subsequent discussion (e.g., the conclusion that azimuthal instabilities appear in the 1 kHz–1 MHz range) relies on them. As a result, the maps cannot be taken as quantitative predictions in those regions. I request either (i) restricting the maximization to kρe < 1 with a statement of how much of the nozzle domain is excluded, or (ii) providing a kinetic or particle-in-cell check of the growth rates at kρe = O(1) for at least the three representative points A–C.
minor comments (6)
- [Section V, paragraph after Fig. V.5] The phrase 'comparing γmax from Figure V.4 with the ones from Figures V.2 and V.3' appears to refer to Figure V.5, not Figure V.4, which is the ω(k) plot for point C.
- [Section II, first paragraph] Typo: 'Consquently' should be 'Consequently'.
- [Figure V.1 caption] Typo: 'thrsuter' should be 'thruster'.
- [Section V, paragraph on point C] The phrase 'as as shown in Figure V.4' should be 'as shown in Figure V.4'.
- [Section III, Eq. (III.7)] The notation 'ωeO(ε)' is ambiguous; please write O(ε ωe) or define the ordering explicitly.
- [Section VI, paragraph after Eq. (VI.8)] The wording 'the second order electron flux has the same sign of the second order velocity ⟨u⊥e1h∗⟩' is confusing because the preceding sentences describe the two terms as having opposite directions; please clarify the sign convention.
Circularity Check
No significant circularity: the dispersion relation is derived algebraically from the fluid equations; the envelope-shape assumption is a modeling premise, not an input that the predictions reduce to.
full rationale
The paper's derivation chain is self-contained. The low-frequency dispersion relation Eq. (III.30) follows algebraically from the linearized electron equations (II.6)-(II.9), the ion solution (II.12)-(II.13), and quasineutrality, with no parameter fitted to the phenomena it predicts. The instability criteria (IV.5)-(IV.7) and the quasi-linear flux (VI.8) are obtained by algebraic manipulation of this dispersion relation and the linearized response; simulation data from Ref. [37] are used only as equilibrium input profiles, not to tune the theory, and the experimental comparisons are qualitative post hoc statements. The only notable modeling choice is the imposed envelope shape Eq. (III.24), selected so that the collisionless dispersion relation appears as a real polynomial in omega_i and justified in Appendix B by a 1D WKB analogy. This is an a priori consistency constraint on the perturbation envelope, not a fitted parameter and not a consequence of the linearized initial-value problem. If the physical envelope differs, the stability criteria would not apply, but that is a validity/robustness concern, not a circular reduction of the predictions to their inputs. Self-citations in the paper are either data sources ([37]), a preliminary conference version ([38]), or background fluid/gradient literature ([11], [45], [46]); none is load-bearing in the sense of importing a uniqueness theorem or an unverified ansatz to forbid alternatives. The central claim—parallel equilibrium gradients can drive instabilities at k_parallel = 0—is derived, not assumed.
Assumptions & free parameters
assumptions (7)
- domain assumption Electrostatic perturbations with B1 = 0.
- domain assumption Isothermal perturbations, Te1 = 0.
- domain assumption Low-frequency ordering ωe = O(ωce ε) and uθe0 = O(ce ε).
- domain assumption Weakly inhomogeneous plasma: second-order spatial derivatives of perturbed quantities are neglected.
- ad hoc to paper The envelope gradient ∇∥ ln(n0φ1/B) obeys Eq. (III.24), chosen so the collisionless dispersion relation is real.
- domain assumption Quasineutrality closure hi1 = he1.
- domain assumption The equilibrium plasma profiles from the HYPHEN-EPT simulation [37] are representative of a real magnetic nozzle.
Cite this review
Pith. "Pith review of Lower-Hybrid Drift Instabilities in a magnetic nozzle." pith.science (2026). https://pith.science/paper/4M5XOCVY
@misc{pith2026241210070,
author = {Pith},
title = {Pith review of: Lower-Hybrid Drift Instabilities in a magnetic nozzle},
year = {2026},
howpublished = {\url{https://pith.science/paper/4M5XOCVY}},
note = {Machine review of arXiv:2412.10070}
}
abstract
Magnetic nozzles are a key component of electrodeless plasma thrusters, acting as their main acceleration stage. Non-stationary phenomena common to the entire range of $E \times B$ devices, such as oscillations and instabilities, are likely to exist in the magnetic nozzle, according to the mounting experimental evidence. These mechanisms could lead to anomalous cross-field transport, either enhancing the plasma plume divergence or favoring electron detachment. In this work we present a local linear analysis of fluid instabilities relevant for said devices, expanding on previous works with the addition of plasma inhomogeneities in the direction parallel to the magnetic field, with a rigorous inclusion of the effects of magnetic curvature, finite Larmor radius and $3$D wave propagation, allowing for a general formulation of drift-driven instabilities in partially magnetized plasmas. Instability conditions are first studied analytically, and then applied to simulation data of a helicon plasma thruster. Finally, the effect of instabilities on wave-driven cross-field electron transport is assessed by means of quasi-linear analysis. This study predicts the onset of essentially-azimuthal instabilities in the $1$ kHz--$1$ MHz range, in qualitative agreement with some of the available experimental data, and highlights the importance of including parallel inhomogeneities in the formulation of the dispersion relation of an $E \times B$ plasma, as these gradients may drive instabilities even in the absence of axial propagation. Lastly, quasi-linear analysis suggests that the induced cross-field transport acts to smooth out the zeroth-order drifts which cause the plasma to destabilize in the first place.
Reference graph
Works this paper leans on
-
[1]
Long-wavelength limit Taking the limit kρe → 0 of relation (IV .7), the instability criterion simplifies to: " ∆ − ωMe − ωTe − Ω2 ∥ ∆∥ # " ωMe + Ω2 ∥ ∆∥ # > 0 . (IV .8) This expression can be easily shown to be a generalization of the MSHI and the MTSI conditions, Eqs. (III.31)-(III.32). Neglecting parallel propagation and gradients, Ω∥ = 0, Eq. (IV .8) y...
-
[2]
Finite Larmor radius effects As kρe becomes non-negligible, rearranging the relation (IV .7) yields a finite Larmor radius correction to the criterion in (IV .8): " ∆ − ωMe − ωTe − Ω2 ∥ ∆∥ # " ωMe + Ω2 ∥ ∆∥ # > − k2ρ2 e " ωTe 2 − ∆ ∆ − ωMe − Ω2 ∥ ∆∥ ! + ∆ ωMe + Ω2 ∥ ∆∥ ! k2ρ2 e 4 + ∆ ωTe 2 − ∆ k4ρ4 e 2 # , (IV .11) implying that even if the condition for ...
work page 2020
-
[3]
E. Ahedo, “Plasmas for space propulsion,” Plasma Physics and Controlled Fusion, vol. 53, no. 12, p. 124037, 2011
work page 2011
-
[4]
Ex- perimental characterization of a 1 kW helicon plasma thruster,
J. Navarro-Cavallé, M. Wijnen, P. Fajardo, and E. Ahedo, “Ex- perimental characterization of a 1 kW helicon plasma thruster,” Vacuum, vol. 149, pp. 69–73, 2018
work page 2018
-
[5]
Technology of closed-drift thrusters,
H. Kaufman, “Technology of closed-drift thrusters,” AIAA Journal, vol. 23, pp. 78–87, 1985
work page 1985
-
[6]
D. Goebel and I. Katz, Fundamentals of Electric Propulsion: Ion and Hall Thrusters . Jet Propulsion Laboratory, Pasadena, CA, 2008
work page 2008
-
[7]
Perspectives on physics of exb discharges relevant to plasma propulsion and similar technolo- gies,
I. D. Kaganovich, A. Smolyakov, Y . Raitses, E. Ahedo, I. G. Mikellides, B. Jorns, F. Taccogna, R. Gueroult, S. Tsikata, A. Bourdon, J.-P. Boeuf, M. Keidar, A. T. Powis, M. Merino, M. Cappelli, K. Hara, J. A. Carlsson, N. J. Fisch, P. Chabert, I. Schweigert, T. Lafleur, K. Matyash, A. V . Khrabrov, R. W. Boswell, and A. Fruchtman, “Perspectives on physics...
work page 2020
-
[8]
Drift ballooning instabilities in tokamak edge plasmas,
R. Hastie, J. Ramos, F. Porcelli, M. o. T. Science, and F. Cen- ter, “Drift ballooning instabilities in tokamak edge plasmas,” Physics of Plasmas, vol. 10, no. 11, pp. 4405–4412, 2003
work page 2003
Show all 51 references
-
[9]
H2020 MINOTOR: Magnetic nozzle electron cyclotron resonance thruster,
D. Packan, P.-Q. Elias, J. Jarrige, T. Vialis, S. Correyero, S. Pe- terschmitt, J. Porto-Hernandez, M. Merino, A. Sánchez-Villar, E. Ahedo, G. Peyresoubes, A. Thorinius, S. Denis, K. Hol- ste, P. Klar, S. Scharmann, J. Zorn, M. Bekemans, T. Scalais, E. Bourguignon, S. Zurbach,...
2019
-
[10]
Magnetic nozzles for space plasma thrusters,
M. Merino and E. Ahedo, “Magnetic nozzles for space plasma thrusters,” inEncyclopedia of Plasma Technology(J. L. Shohet, ed.), vol. 2, pp. 1329–1351, Taylor and Francis, 2016
2016
-
[11]
Local analysis of electrostatic modes in a two-fluid E x B plasma,
J. J. Ramos, E. Bello-Benítez, and E. Ahedo, “Local analysis of electrostatic modes in a two-fluid E x B plasma,” Physics of Plasmas, vol. 28, no. 5, p. 052115, 2021
2021
-
[12]
Fluid 19 and kinetic plasma instabilities for hall effect thrusters,
K. Hara, A. R. Mansour, A. C. Denig, and S. Tsikata, “Fluid 19 and kinetic plasma instabilities for hall effect thrusters,” in37th International Electric Propulsion Conference, 2022
2022
-
[13]
Parametric analysis of the two-fluid tearing instability,
E. Ahedo and J. Ramos, “Parametric analysis of the two-fluid tearing instability,” in50th Annual Meeting of the APS-Division of Plasma Physics, November 2008, 2008
2008
-
[14]
Normal-mode-based theory of collisionless plasma waves,
J. J. Ramos, “Normal-mode-based theory of collisionless plasma waves,” Journal of Plasma Physics, 2019
2019
-
[15]
Plasma oscillations in Hall thrusters,
E. Choueiri, “Plasma oscillations in Hall thrusters,” Physics of Plasmas, vol. 8, no. 4, pp. 1411–1426, 2001
2001
-
[16]
Advances on low- dimensionality fluid modelling of Hall thruster discharges,
E. Bello-Benítez and E. Ahedo, “Advances on low- dimensionality fluid modelling of Hall thruster discharges,” in Space Propulsion Conference 2021 , no. paper 133, (March 17-19), Association Aéronautique et Astronautique de France, 2021
2021
-
[17]
Physics and instabilities of low- temperature E x B plasmas for spacecraft propulsion and other applications,
J.-P. Boeuf and A. Smolyakov, “Physics and instabilities of low- temperature E x B plasmas for spacecraft propulsion and other applications,” Physics of Plasmas, vol. 30, no. 5, 2023
2023
-
[18]
Using electron fluid models to analyze plasma thruster discharges,
E. Ahedo, “Using electron fluid models to analyze plasma thruster discharges,” Journal of Electric Propulsion , vol. 2, no. 1, p. 2, 2023
2023
-
[19]
Effect of the magnetic field on a closed-electron- drift accelerator,
A. Morozov, Y . Esipchuk, A. Kapulkin, V . Nevrovskii, and V . Smirnov, “Effect of the magnetic field on a closed-electron- drift accelerator,” Sov. Phys.-Tech. Phys.(Engl. Transl.) 17: No. 3, 482-7 (Sep 1972)., 1972
1972
-
[20]
Drift instability in a Hall-current plasma accelerator,
Y . Esipchuk and G. Tilinin, “Drift instability in a Hall-current plasma accelerator,” Sov. Physics-Tech. Physics, vol. 21, no. 4, pp. 417–423, 1976
1976
-
[21]
Time- dependent axial fluid model of the hall thruster discharge and its plume,
D. Poli, E. Bello-Benítez, P. Fajardo, and E. Ahedo, “Time- dependent axial fluid model of the hall thruster discharge and its plume,” Journal of Physics D: Applied Physics, 2023
2023
-
[22]
Effect of injection conditions on the non-linear behavior of the ECDI and related turbulent transport,
E. Bello-Benítez, A. Marín-Cebrián, and E. Ahedo, “Effect of injection conditions on the non-linear behavior of the ECDI and related turbulent transport,” 2024. Pre-print available at https://arxiv.org/pdf/2405.08761
2024 arXiv
-
[23]
Fluid theory and simulations of instabilities, tur- bulent transport and coherent structures in partially-magnetized plasmas of ExB discharges,
A. Smolyakov, O. Chapurin, W. Frias, O. Koshkarov, I. Ro- madanov, T. Tang, M. Umansky, Y . Raitses, I. Kaganovich, and V . Lakhin, “Fluid theory and simulations of instabilities, tur- bulent transport and coherent structures in partially-magnetized plasmas of ExB discharges,”...
2017
-
[24]
for both electrostatic and electromagnetic waves. Ramos, Bello and Ahedo [11] provided a more general derivation of fluid electrostatic instabilities in E × B plasmas, examining in detail drift-gradient and drift-resisitive instabilities in a variety of frequency and wavelengt...
2024 arXiv
-
[25]
Long wavelength gradient drift instability in Hall plasma devices. I. Fluid theory,
W. Frias, A. Smolyakov, I. Kaganovich, and Y . Raitses, “Long wavelength gradient drift instability in Hall plasma devices. I. Fluid theory,”Physics of Plasmas, vol. 19, p. 072112, 2012
2012
-
[26]
Low frequency azimuthal stability of the ionization region of the hall thruster discharge. i. local analysis,
D. Escobar and E. Ahedo, “Low frequency azimuthal stability of the ionization region of the hall thruster discharge. i. local analysis,” Physics of Plasmas, vol. 21, no. 4, p. 043505, 2014
2014
-
[27]
Low-frequency instabilities in magnetic pulses,
N. A. Krall and P. C. Liewer, “Low-frequency instabilities in magnetic pulses,” Physical Review A , vol. 4, pp. 2094–2103, 1971
1971
-
[28]
Resistive instabilities in Hall current plasma discharge,
A. Litvak and N. Fisch, “Resistive instabilities in Hall current plasma discharge,” Physics of Plasmas, vol. 8, no. 2, pp. 648– 651, 2001
2001
-
[29]
Instability of electrons drifting through ions across a magnetic field,
O. Buneman, “Instability of electrons drifting through ions across a magnetic field,” Journal of Nuclear Energy. Part C, Plasma Physics, Accelerators, Thermonuclear Research, vol. 4, no. 2, pp. 111–117, 1962
1962
-
[30]
Axial-azimuthal, high- frequency modes from global linear-stability model of a Hall thruster,
E. Bello-Benítez and E. Ahedo, “Axial-azimuthal, high- frequency modes from global linear-stability model of a Hall thruster,” Plasma Sources Science and Technology , vol. 30, p. 035003, 3 2021
2021
-
[31]
∆ 1 + k4ρ4 e 4 − ωMe − ωTe − Ω2 ∥ ∆∥ # ×
to the magnetosonic wave in the work of Takahashi et al. [28], the latter being electromagnetic in nature. In the work of Desjardins and Gilmore [33], the oscillations are identified as a mixture of drift-resistive electron drift waves and Kelvin- Helmoltz instabilities. Moreo...
-
[32]
Wave-driven electron inward transport in a magnetic nozzle,
K. Takahashi, C. Charles, and R. W. Boswell, “Wave-driven electron inward transport in a magnetic nozzle,” Scientific re- ports, vol. 12, no. 1, p. 20137, 2022
2022
-
[33]
Experimental characterization of oscillations in the magnetic nozzle of an electron cyclotron res- onance thruster,
D. Maddaloni, F. Boni, V . Désangles, B. Bayón-Buján, M. Merino, and F. Terragni, “Experimental characterization of oscillations in the magnetic nozzle of an electron cyclotron res- onance thruster,” in 38th International Electric Propulsion Con- ference, no. IEPC-2024-387, (T...
2024
-
[34]
Low-frequency oscillations in the magnetic noz- zle of a helicon plasma thruster,
D. Maddaloni, B. Bayón-Buján, J. Navarro-Cavallé, and M. Merino, “Low-frequency oscillations in the magnetic noz- zle of a helicon plasma thruster,” Plasma Sources Scinece and Technology (under review), 2024
2024
-
[35]
Wave-driven non-classical electron transport in a low temperature magnetically expanding plasma,
S. Hepner, B. Wachs, and B. Jorns, “Wave-driven non-classical electron transport in a low temperature magnetically expanding plasma,” Applied Physics Letters, vol. 116, no. 26, p. 263502, 2020
2020
-
[36]
A. E. Vinci, Physics of magnetic nozzles and helicon plasma discharges. PhD thesis, Université d’Orléans, 2022
2022
-
[37]
Dynamics of flows, flucua- tions, and global instability under electrode biasing in a linear plasma device,
T. R. Desjardins and M. Gilmore, “Dynamics of flows, flucua- tions, and global instability under electrode biasing in a linear plasma device,” Physics of Plasmas, 2016
2016
-
[38]
Effects of a magnetic field gradi- ent on the lower hydrid drift instability,
J. D. Huba and C. S. Wu, “Effects of a magnetic field gradi- ent on the lower hydrid drift instability,”The Physics of Fluids, vol. 19, no. 7, pp. 988–994, 1976
1976
-
[39]
In what sense do slow waves carry negative energy?,
P. A. Sturrock, “In what sense do slow waves carry negative energy?,” Journal of Applied Physics, vol. 31, no. 11, 1960
1960
-
[40]
Hasegawa, Plasma Instabilities and Nonlinear Effects
A. Hasegawa, Plasma Instabilities and Nonlinear Effects . Springer-Verlag, 1975
1975
-
[41]
Analysis of a cusped helicon plasma thruster discharge,
P. Jiménez, J. Zhou, J. Navarro-Cavallé, P. Fajardo, M. Merino, and E. Ahedo, “Analysis of a cusped helicon plasma thruster discharge,” Plasma Sources Science and Technology , vol. 32, no. 10, p. 105013, 2023
2023
-
[42]
Analysis of drift in- stabilities in magnetic nozzles,
M. Ripoli, M. Merino, and E. Ahedo, “Analysis of drift in- stabilities in magnetic nozzles,” in 38 th International Elec- tric Propulsion Conference , no. IEPC-2024-506, (Toulouse, France, June 23-28), Electric Rocket Propulsion Society, 2024
2024
-
[43]
Con- tinuous supersonic plasma wind tunnel,
S. Andersen, V . Jensen, P. Nielsen, and N. D’Angelo, “Con- tinuous supersonic plasma wind tunnel,” Phys. Fluids, vol. 12, no. 3, pp. 557–560, 1969
1969
-
[44]
Two-dimensional supersonic plasma acceleration in a magnetic nozzle,
E. Ahedo and M. Merino, “Two-dimensional supersonic plasma acceleration in a magnetic nozzle,”Physics of Plasmas, vol. 17, no. 7, p. 073501, 2010
2010
-
[45]
Time-dependent expansion of a weakly-collisional plasma beam in a paraxial magnetic nozzle,
J. Zhou, G. Sánchez-Arriaga, and E. Ahedo, “Time-dependent expansion of a weakly-collisional plasma beam in a paraxial magnetic nozzle,” Plasma Sources Science and Technology , vol. 30, no. 4, p. 045009, 2021
2021
-
[46]
General expression of the gyroviscous force,
J. Ramos, “General expression of the gyroviscous force,” Physics of Plasmas, vol. 12, no. 11, p. 112301, 2005
2005
-
[47]
The universally growing mode in the solar atmosphere: coronal heating by drift waves,
J. Vranjes and S. Poedts, “The universally growing mode in the solar atmosphere: coronal heating by drift waves,” Monthly Notices of the Royal Astronomical Society, 2009
2009
-
[48]
Nonlinear plasma theory,
R. Z. Sagdeev, A. A. Galeev, T. M. O’Neil, and D. L. Book, “Nonlinear plasma theory,” 1969
1969
-
[49]
Magnetized fluid electron model within a two-dimensional hybrid simulation code for electrodeless plasma thrusters,
J. Zhou, A. Domínguez-Vázquez, P. Fajardo, and E. Ahedo, “Magnetized fluid electron model within a two-dimensional hybrid simulation code for electrodeless plasma thrusters,” Plasma Sources Science and Technology , vol. 31, no. 4, p. 045021, 2022
2022
-
[50]
Hybrid plasma simula- tions of the HT5k thruster,
J. Perales-Díaz, A. Domínguez-Vázquez, P. Fajardo, E. Ahedo, F. Faraji, M. Reza, and T. Andreussi, “Hybrid plasma simula- tions of the HT5k thruster,” in ExB Plasmas Workshop, Young researchers "poster" mini-session , (Madrid, Spain, February 16-18), 2022
2022
-
[51]
T. H. Stix, Waves in plasmas . Springer Science & Business Media, 1992
1992
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