Abstract:Plasma propulsion concepts that employ a guiding magnetic field raise the question of how the magnetically controlled plasma can detach from the spacecraft. This paper presents a detachment scenario relevant to high-power thrusters in which the plasma can stretch the magnetic field lines to infinity, similar to the solar wind. In previous work, the corresponding ideal magnetohydrodynamics equations have been solved analytically for a plasma flow in a slowly diverging nozzle. That solution indicates that effici… Show more
“…When β becomes larger than unity, typically the field-lines cannot collimate the plasma because selfconsistent effects drive the plasma across field-lines [12]. For the injected kinetic stabilizer ions, the local β ks = 2µ 0 p/B 2 must be less than unity along the imposed field-lines.…”
Section: Beta Limitation and Adiabaticity Limitsmentioning
A kinetically stabilized axially symmetric tandem mirror (KSTM) uses the momentum flux of low-energy, unconfined particles that sample only the outer end-regions of the mirror plugs, where large favorable field-line curvature exists. The window of operation is determined for achieving MHD stability with tolerable energy drain from the kinetic stabilizer. Then MHD stable systems are analyzed for stability of the trapped particle mode. This mode is characterized by the detachment of the central-cell plasma from the kinetic stabilizer region without inducing field-line bending. Stability of the trapped particle mode is sensitive to the electron connection between the stabilizer and the end plug. It is found that the stability condition for the trapped particle mode is more constraining than the stability condition for the MHD mode, and it is challenging to satisfy the required power constraint. Furthermore a severe power drain may arise from the necessary connection of low-energy electrons in the kinetic stabilizer to the central region.
“…When β becomes larger than unity, typically the field-lines cannot collimate the plasma because selfconsistent effects drive the plasma across field-lines [12]. For the injected kinetic stabilizer ions, the local β ks = 2µ 0 p/B 2 must be less than unity along the imposed field-lines.…”
Section: Beta Limitation and Adiabaticity Limitsmentioning
A kinetically stabilized axially symmetric tandem mirror (KSTM) uses the momentum flux of low-energy, unconfined particles that sample only the outer end-regions of the mirror plugs, where large favorable field-line curvature exists. The window of operation is determined for achieving MHD stability with tolerable energy drain from the kinetic stabilizer. Then MHD stable systems are analyzed for stability of the trapped particle mode. This mode is characterized by the detachment of the central-cell plasma from the kinetic stabilizer region without inducing field-line bending. Stability of the trapped particle mode is sensitive to the electron connection between the stabilizer and the end plug. It is found that the stability condition for the trapped particle mode is more constraining than the stability condition for the MHD mode, and it is challenging to satisfy the required power constraint. Furthermore a severe power drain may arise from the necessary connection of low-energy electrons in the kinetic stabilizer to the central region.
“…Other investigations, such as that found in Ref. [1], discuss the far-field region. Nevertheless, observations of plasma behavior in the near-field of the magnetic nozzle have proved to be informative and the results from this simulation can be extrapolated to estimate far-field behavior and can yield self-consistent boundary conditions for far-field simulations.…”
Section: Discussionmentioning
confidence: 95%
“…However, due to the solenoidal nature of the magnetic field it is essential to ensure that the plasma detaches from the field, making this a problem of active research. 1,2 While other investigations have looked into far-field phenomena, like detachment, this paper discusses numerical simulations of the near-field behavior of plasma jets in magnetic nozzles, where the applied field gradients are greatest. The development of a multidimensional numerical tool that can be used to investigate plasma detachment mechanisms was introduced in Ref.…”
The development and application of a multidimensional numerical simulation code for investigating nearfield plasma processes in magnetic nozzles are presented. The code calculates the time-dependent evolution of all three spatial components of both the magnetic field and velocity in a plasma flow, and includes physical models of relevant transport phenomena. It has been applied to an investigation of the behavior of plasma flows found in high-power thrusters, employing a realistic magnetic nozzle configuration. Simulation of a channelflow case where the flow was super-Alfvénic has demonstrated that such a flow produces adequate 'back-emf' to significantly alter the shape of the total magnetic field, preventing the flow from curving back to the magnetic field coil in the near-field region. Results from this simulation can be insightful in predicting far-field behavior and can be used as a set of self-consistent boundary conditions for far-field simulations. Future investigations will focus on cases where the inlet flow is sub-Alfvénic and where the flow is allowed to freely expand in the radial direction once it is downstream of the coil.
“…Arefiev and Breizman describe magnetized ideal MHD flow constrained to be field-directed everywhere and characterize successful detachment by the transition of plasma flow from a sub-Alfvénic to a super-Alfvénic regime [1,2]. Physically, the detached plume is said to stretch the frozen-in magnetic field lines to infinity.…”
Section: Introductionmentioning
confidence: 99%
“…Several models have been proposed to describe the physics of magnetic plasma detachment [1][2][3][4]. Arefiev and Breizman describe magnetized ideal MHD flow constrained to be field-directed everywhere and characterize successful detachment by the transition of plasma flow from a sub-Alfvénic to a super-Alfvénic regime [1,2].…”
Abstract. The model of two-fluid, axisymmetric, ambipolar magnetized plasma detachment from thruster guide fields is extended to include plasmas with non-zero injection angular velocity profiles. Certain plasma injection angular velocity profiles are shown to narrow the plasma plume, thereby increasing exhaust efficiency. As an example, we consider a magnetic guide field arising from a simple current ring and demonstrate plasma injection schemes that more than double the fraction of useful exhaust aperture area, more than halve the exhaust plume angle, and enhance magnetized plasma detachment.
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