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6. Research on the neutralization control of the rf ion micropropulsion system for the ‘Taiji-1’ satellite mission
10.1088/2058-6272/ab7dd5 ↗9. Perspectives, frontiers, and new horizons for plasma-based space electric propulsion
10.1063/1.5109141 ↗10. Diversity of physical processes: Challenges and opportunities for space electric propulsion
10.3390/app122111143 ↗14. History of the hall thrusters development in ussr
15. A critical history of electric propulsion: The first 50 years (1906-1956)
10.2514/1.9245 ↗18. High-specific impulse hall thrusters, part 2: Efficiency analysis
10.2514/1.15954 ↗19. High-specific impulse hall thrusters, part 1: Influence of current density and magnetic field
10.2514/1.15952 ↗22. Effects of the radial plasma-wall interaction on the hall thruster discharge
10.1063/1.1584432 ↗25. Stationary plasma thruster (SPT) development steps and future perspectives
26. Modeling an anode layer Hall thruster and its plume
27. Main physical features and processes determining the performance of stationary plasma thrusters
10.2514/2.5335 ↗28. Review of hall thruster neutral flow dynamics
31. Low frequency azimuthal stability of the ionization region of the hall thruster discharge. I. Local analysis
10.1063/1.4870963 ↗33. Effect of density inhomogeneity in azimuth on discharge oscillation suppression and electron diffusion in hall thrusters
34. Direct evidence of gradient drift instability being the origin of a rotating spoke in a crossed field plasma
10.1088/1361-6595/ac0487 ↗37. The influence of neutral flow rate in the operation of hall thrusters
42. Investigation of the anode configuration influence on the pps-1350 laboratory model plume divergence
46. Experimental optimization of small krypton hall thruster for operation at high voltage
47. Development and testing of a 4500 watt flight type hall thruster and cathode
48. Design and experiments of a 100 watt magnetically shielded hall thruster
50. Xenon gas injection in SPT thrusters
51. Influence of propellant-inlet condition on hall thruster performance
53. Study of plasma dynamics in the variable section channel stationary plasma thruster
55. Study on ionization characteristics of low power hall thruster with variable cross-section channel
56. Effect of oblique channel on discharge characteristics of 200-w hall thruster
10.1063/1.4976104 ↗58. Numerical simulation study on the influence of channel geometry on discharge characteristics of low-power magnetically shielded hall thrusters
10.1016/j.vacuum.2020.109547 ↗61. Numerical investigation of reversed gas feed configurations for hall thrusters
10.2514/1.b38346 ↗62. Investigation of short-channel design on performance optimization effect of hall thruster with large height–radius ratio
10.1088/2058-6272/ac44f1 ↗63. Experimental and numerical simulation study of the effect for the anode positions on the discharge characteristics of 300 W class low power hall thrusters
10.1088/2058-6272/ac7d42 ↗66. Effect of magnetic field directionality on discharging characteristics of hall effect thruster with azimuthal diversion rail
10.1116/1.5037215 ↗68. Laser-induced fluorescence study of neutral xenon flow evolution inside a 6-kW hall thruster
69. Laser-induced fluorescence of neutral xenon in the near field of a 200 W hall thruster
70. Near-plume laser-induced fluorescence velocity measurements of a medium power hall thruster
10.2514/1.44411 ↗71. Lif-Doppler velocity measurement of xenon atoms in a SPT-50
72. The H9 magnetically shielded hall thruster
73. Performance characterization of a low-power magnetically shielded hall thruster with an internally-mounted hollow cathode
10.1088/1361-6595/ab47de ↗74. Development and initial performance testing of a low-power magnetically shielded hall thruster with an internally-mounted hollow cathode
75. Gridded retarding pressure sensor for ion and neutral particle analysis in flowing plasmas
10.1063/1.1147881 ↗76. The gear of a working gas flow in the SPT discharge chamber
77. Characterization of hall effect thruster propellant distributors with flame visualization
10.1063/1.4774049 ↗78. Images of ground state xenon density in the near field of a low power hall thruster
79. Temperature of xenon atoms in a stationary plasma thruster
83. Propellant thermal management effect on neutral residence time in low-voltage hall thrusters
10.2514/1.b34702 ↗84. Development and characterization of high -efficiency, high -specific impulse xenon hall thrusters
85. Azimuthal non-uniformities in accelerators with closed electron drift
86. Discharge characteristics and increased electron current during azimuthally nonuniform propellant supply in an anode layer hall thruster
10.1063/1.5144851 ↗88. Discharge stabilization method of an anode layer type hall thruster by non-uniform propellant flow
89. Effects of azimuthal non-uniformity on the hall thruster discharge
90. Plasma formation and cross-field electron transport induced by azimuthal neutral inhomogeneity in an anode layer hall thruster
10.1063/1.5090931 ↗91. Evolution of electron cross-field transport induced by an equilibrium azimuthal electric field in an E × B hall thruster discharge under an azimuthally inhomogeneous neutral supply
10.1063/5.0060377 ↗93. Hall thruster performances using low cost propellant
96. Efficiency analysis of a hall thruster operating with krypton and xenon
10.2514/1.19613 ↗97. Influence of xenon and krypton flow rates through the acceleration channel of Morozov’s stationary plasma thruster on the thrust efficiency
10.1134/s1063780x19010082 ↗100. Preliminary characterization test of het and rit with nitrogen and oxygen