Experimental study of ATON stationary plasma thrusters

Results from experimental studies of integral characteristics of laboratory models of second-generation ATON stationary plasma thrusters are presented. Special attention is paid to high-voltage modes with a sufficiently high specific anode propulsive burn. Integral parameters of the thrusters were measured using a test bench with diffusion evacuation at the Moscow State Institute of Radioengineering, Electronics, and Automation and that with cryogenic evacuation at the Fakel Experimental and Design Bureau. The values of the thrust, specific propulsive burn, and efficiency measured in these test benches in the main operating mode coincide to within measurement errors. At a discharge power of 2 kW and voltage of about 700 V, the specific anode propulsive burn and anode thrust efficiency reach 3000 s and 60%, respectively. The experimental data show that the efficiency of the ATON stationary plasma thruster operating in a high-voltage mode is higher than that of other similar thrusters.     

Model of the near-wall conductivity in the vicinity of a macroscopically inhomogeneous, mirror-reflecting surface

A study is made of the interaction of the electron component of a low-density plasma with a macroscopically inhomogeneous, mirror-reflecting surface in mutually orthogonal electric and magnetic fields. The collisionless kinetic equation is solved analytically in the (2R+3V)-dimensional space. A nontrivial structure of the nascent near-wall currents is revealed, and their two-dimensional distribution is analyzed in detail. From the standpoint of practical applications, attention is focused on the near-wall conductivity in a stationary plasma thruster. The results obtained agree with the available experimental data. Moreover, the investigations described here provide a basis for the study of the possibility of tailoring the insulator in the channel for the purpose of suppressing anomalous erosion and ensuring the required operating period of plasma thrusters. __________ Translated from Fizika Plazmy, Vol. 28, No. 2, 2002, pp. 180–187. Original Russian Text Copyright ￠ 2002 by Kozlov.     

Global characteristics of an ATON stationary plasma thruster operating with krypton and xenon

The global characteristics of an ATON stationary plasma thruster operating on xenon and krypton are investigated. It is shown that, with krypton, the thrust at the same mass flow rate of the working gas is greater and the efficiency is somewhat lower than those with xenon. An efficiency of ～60% was achieved with krypton for the specific impulse attaining 3000 s. The jet divergence is ～±22° for krypton and ～±11° for xenon.     

Formation of charge-exchange ion flows near the exit from the stationary plasma thruster acceleration channel

Ion currents onto the exit plane of the acceleration channel of a stationary plasma thruster model were measured using electrostatic probes the collecting surfaces of which could be oriented either upstream or downstream with respect to the thruster plume. Using the results of measurements, the so-called “back” flows of charge-exchange ions onto the exit plane are estimated. It is shown that the back ion flows are the most intense in the close vicinity of the thruster, but do not exceed 0.6% of the total ion flow from the thruster. The formation of steady-state ion flows near the exit from the acceleration channel of a stationary plasma thruster is simulated numerically by using a three-dimensional kinetic model that describes the dynamics of ions and neutral atoms exhausting from the acceleration channel and produced in the thruster plume and takes into account resonance charge exchange of ions with neutral atoms. The distribution of the back ion current density in the exit plane is determined. The effect of the flow rate of the working gas through the cathode on the distributions of the neutral atom density and charge-exchange ion flows is demonstrated. The obtained results can be used to analyze the effect of the thruster plume on the charge state of the surfaces located in the vicinity of the thruster.     

A simple model to determine the interrelation between the integral characteristics of hall thrusters

A simple model to determine the interrelation between the integral characteristics of Hall thrusters with an anode layer is proposed. The model includes the equation describing the balance of forces acting on the Hall current region, as well as the relationship between the current of accelerated ions and the rate of working gas consumption. For fixed geometrical characteristics of a specific Hall thruster, this model allows one to interrelate the main integral characteristics of the thruster, such as the accelerating voltage, the magnetic field, the propellant flow rate, and the current of accelerated ions. The results of calculations for TAL-WSF/D-55—one of the most widely used Hall thrusters with an anode layer—are presented. The domain of existence of the discharge in the channel of the Hall thruster is analyzed. It is shown that taking into account kinetic effects of neutral particle expansion and working gas preheating lead to a decrease in the current of accelerated ions and the engine thrust.     

Nonstationary Model of a Low-Density Plasma Jet Ejected from a Stationary Plasma Thruster

A time-dependent problem on finding the parameters of a low-density plasma jet ejected from a stationary plasma thruster is analyzed. In contrast to earlier works in which a stationary problem was solved using a Crook-type kinetic model, a set of kinetic equations is derived at the accuracy level accepted in the kinetic theory with allowance for resonant charge-exchange interaction between ions and neutrals. A method to solve the obtained set of equations is developed and used to perform test simulations, some results of which are presented.     

Microwave processes in the SPD-ATON stationary plasma thruster

Results of experimental studies of microwave processes accompanying plasma acceleration in the SPD-ATON stationary plasma thruster are presented. Specific features of the generation of microwave oscillations in both the acceleration channel and the plasma flow outgoing from the thruster are analyzed on the basis of local measurements of the spectra of the plasma wave fields. Mechanisms for generation of microwave oscillations are considered with allowance for the inhomogeneity of the electron density and magnetic field behind the edge of the acceleration channel. The effect of microwave oscillations on the electron transport and the formation of the discharge current in the acceleration channel is discussed.     

Measurements of a negative ion flux inplasma thruster tests in a vacuum chamber

The dynamics of negative ions created in the interaction of a plasma jet with a target is investigated experimentally. The experiments were carried out with a stationary plasma thruster. A multigrid probe was used to record negative ions.     

Discharge Oscillations in Morozov’s Stationary Plasma Thruster as a Manifestation of Large-Scale Modes of Gradient Drift Instability

Plasma Physics Reports - The phenomenon of large-scale discharge oscillations in Morozov’s stationary plasma thruster (SPT) is physically interpreted by analyzing global modes of gradient...     

Stability of Ion Flow and Role of Boundary Conditions in a Simplified Model of the E × B Plasma Accelerator with a Uniform Electron Mobility

Plasma Physics Reports - Resistive oscillations of axial plasma with ionization effects are analyzed in configuration similar to the Hall effect thrusters. From analysis of stationary equations we...     

Experimental study on the structure of high-frequency perturbations near the exit plane of a stationary plasma thruster with a high specific impulse

Results from experimental studies of the structure of high-frequency waves near the exit plane of a stationary plasma thruster are presented. The role played by such waves in the electron transport across the magnetic field is discussed on the basis of the obtained experimental data.     

Influence of Xenon and Krypton Flow Rates through the Acceleration Channel of Morozov’s Stationary Plasma Thruster on the Thrust Efficiency

Plasma Physics Reports - Morozov’s stationary plasma thrusters (SPTs) operating with xenon have been successfully used for many years in space technology. At the same time, due to the high...     

Electron energy balance and ionization in the channel of a stationary plasma thruster

The paper presents results of numerical simulations of the electron dynamics in the field of the azimuthal and longitudinal waves excited in the channel of a stationary plasma thruster (SPT). The simulations are based on the experimentally determined wave characteristics. The simulation results show that the azimuthal wave displayed as ionization instability enhances electron transport along the thruster channel. It is established that the electron transport rate in the azimuthal wave increases as compared to the rate of diffusion caused by electron scattering from neutral atoms in proportion to the ratio between the times of electron? neutral collisions responsible for ionization and elastic electron scattering, respectively. An expression governing the plasma conductivity is derived with allowance for electron interaction with the azimuthal wave. The Hall parameter, the electron component of the discharge current, and the electron heating power in the thruster channel are calculated for two model SPTs operating with krypton and xenon. The simulation results agree well with the results of experimental studies of these two SPTs.     

Determination of fluvastatin and its five metabolites in human plasma using simple gradient reversed-phase high-performance liquid chromatography with ultraviolet detection

A simple gradient reversed-phase high-performance chromatographic method with ultraviolet detection for the determination of fluvastatin (FV) and its five metabolites, (M-2, M-3, M-4, M-5 and M-7) in human plasma was developed and validated. The limit of quantification of FV and its five metabolites in human plasma was 10 ng ml⁻¹. The assay had satisfactory selectivity, recovery, linearity and precision accuracy. Stability studies showed that FV and its five metabolites were stable in plasma up to at least 1 month of storage at −30°C.     

Plasma electron-emitting source in a low-pressure beam-plasma discharge in a stationary plasma thruster

A new type of plasma electron-emitting source capable of increasing the temperature of plasma electrons behind the edge of a stationary plasma thruster (SPT) to 7–15 eV has been developed and investigated experimentally. For the same parameters of the main discharge, the thrust, the thrust efficiency, the mass use factor, and the lifetime of the “SPT anode unit-plasma electron-emitting source” assembly are found to increase substantially as compared to a thruster equipped with a conventional cathode compensator. Simultaneously, the neutral particle pressure required for the existence of self-consistent distributions of the electric field and charged particle density in the drift space of the neutralized ion beam decreases appreciably. It is shown that the volume of the region in which primary slow ions are produced increases with increasing ionization frequency. Three additional channels for discharge control are implemented. The ranges in which the discharge parameters can be controlled are extended.     

The response of two rice cultivars to external Na/Ca ratio

The response of the rice cultivars ‘M9’ and ‘M-201’ to nutrient cultures salinated at −0.4 MPa with varying ratios of Na and Ca was studied. Although the dry matter production of both cultivars was sensitive to the Na/Ca ratio, this correlation was significant only for M-201. Calcium nutrition was severely affected by the composition of the external solution, and the laminae exhibited Ca-deficiency symptoms at Na/Ca molar ratios of 78 and 198. Sodium concentration in the shoot decreased as the Na/Ca ratio in the external solution decreased. Patterns of Na and Cl distribution in the shoot tissues were similar; both ions were accumulated preferentially in the tillers and older leaves. The Na-induced inhibition of Ca uptake and transport appears to be more limiting to shoot growth of M9 and M-201 than Na toxicity per se.     

Quantifying the extent of niche areas in the global fleet of commercial ships: the potential for “super-hot spots” of biofouling

Niche areas of ships, such as lateral thruster tunnels, sea chests, and propellers, are often hot spots for the accumulation of biofouling organisms, a potential source of aquatic invasive species. Yet, the relative importance of different niche areas is poorly resolved, in terms of both total surface area and the associated biota (i.e., the species of organisms and their abundances). To address this information gap, a method was developed to estimate the extent of various niche areas in the global fleet of 120,252 commercial ships active between 1999 and 2013. The total niche area for these vessels was estimated to be 32,996 × 10³ m², representing approximately 10% of the total wetted surface area (WSA) available for colonization by biota. Considering the portion of niche areas relative to the total WSA, it was highest for passenger vessels (27%), followed by tugs (25%), and fishing vessels (21%), with niche areas representing a small portion of the WSA for bulk carriers and tankers (7–8%). Examining the different types of niche areas, thruster tunnels had the greatest total extent (10,189 × 10³ m²), representing a disproportionately large contribution (>50%) of the total niche area for passenger vessels and tugs compared to other vessel types. This result, combined with the use and cleaning of thrusters, may render them “super-hot spots” of biofouling. The uneven distribution and extent of niche areas across vessels has implications for transfers of organisms and management strategies to reduce invasions associated with the surfaces of ships.     

The conceptual development of stationary plasma thrusters

The history of the development of the concept of the stationary plasma thruster is described. The data obtained indicate the possibility of creating extended (over a distance substantially longer than the Debye radius) electric fields in a fully ionized plasma with a relatively high electron temperature (T_e>10 eV) and a conductivity close to the classical one. Based on these results, a number of fundamentally new plasma-dynamic systems were proposed; in particular, the principles of plasma optics were formulated and verified experimentally. In the course of these investigations, new physical processes, such as the formation of the distribution function of the electrons in their collisions with the wall and the effect of the near-wall conductivity, were discovered. The structure of the Debye layer for the case in which the coefficient of the secondary electron emission of a dielectric wall is larger than unity was investigated.     

The effect of estradiol benzoate on synchrony of estrus and fertility in cattle after removal of a progesterone-releasing intravaginal device.

The aim was to determine the effect of estradiol benzoate (EDB) given after removal of a progesterone-releasing intravaginal device (PRID) at either emergence or dominance of a follicle wave, on the interval to estrus, variation in its onset and pregnancy rate in heifers. Heifers (n=186) were assigned randomly to four treatments in a 2 x 2 factorial design; emergence or dominance of a follicle wave at PRID removal, with or without 0.5 mg EDB 24 h after PRID removal. Ovarian ultrasonography was performed to confirm follicular status; data from heifers of undeterminable follicular status were excluded (n=36). Mean size of the largest follicle of the new wave at PRID removal was smaller (P < 0.01) in heifers given EDB at emergence (6.3 +/- 0.09 mm) compared with those given it at dominance (10.9 +/- 0.30 mm). The onset of estrus was earlier (P < 0.01) in heifers given EDB at dominance (median 42 h, range 13 h) compared with those not given EDB at dominance (median 43 h, range 42 h). The median interval to estrus was decreased (P < 0.01) in heifers given EDB at emergence (median 48 h, range 73 h) compared with those not given EDB at emergence (median 66 h, range 45 h). Variation in onset of estrus was reduced (P < 0.05) in heifers given EDB compared with those not given EDB. The pregnancy rate was not affected when EDB was given at dominance, however, it was decreased (P < 0.05) when given at emergence (23 of 40 vs 26 of 32, respectively). To determine the effect of EDB on follicular dynamics in heifers treated with EDB at emergence, heifers (n=37) were assigned to two treatments: at emergence with or without EDB and their ovaries were examined daily using ultrasonography. Follicular dynamics were not different (P > 0.05) in EDB-heifers compared with untreated controls. Mean serum estradiol was greater (P < 0.01) in EDB-treated heifers compared with controls. In conclusion, 0.5 mg EDB given 24 h after PRID removal to heifers decreased the interval to estrous onset at emergence or dominance, decreased variation in onset of estrus and decreased pregnancy rates when given at emergence of a follicle wave.