|
Home
>
Journal Issues
>
No 4 (2020) Technical mechanics
>
10
___________________________________________________
UDC 533.9
Technical mechanics, 2020, 4, 97 - 108
Mathematical modeling of probe measurements in a supersonic flow of a four-component collisionless plasma
DOI:
https://doi.org/10.15407/itm2020.04.097
Lazuchenkov D. N., Lazuchenkov N. M.
Lazuchenkov D. N.
Institute of Technical Mechanics of the National Academy of Sciences of Ukraine and the State Space Agency of Ukraine
Lazuchenkov N. M.
Institute of Technical Mechanics of the National Academy of Sciences of Ukraine and the State Space Agency of Ukraine
The aim of this work is the development of a procedure for extracting the plasma electron density and
temperature and ion composition from the current-voltage characteristic (C –V characteristic) of an
isolated probe system of cylindrical electrodes. The plasma is four-component and consists of
electrons, ions of two species with significantly different masses, and neutrals. The measuring
probe and the reference electrode of the probe system may be made up of several cylinders. The
electrodes of the probe system are placed transversely to a supersonic flow of a low-temperature
collisionless plasma with a specified mass velocity.
Using the familiar theoretical and experimental relationships for the ion and electron currents to
a cylinder, a mathematical model of current collection is constructed for an isolated probe system
at an arbitrary ratio of the electrode surface areas. The model includes the calculation of the
equilibrium potential of the reference electrode as a function of the probe bias voltage. A procedure
is developed for the identification of local plasma parameters using a priori information on the
plasma properties and the experimental conditions. The effect of the electron density and temperature
and the ion composition on the probe current of the isolated probe system at different ratios of the
current-collecting electrode surface areas is studied. The ranges of the probe bias potentials and
the values of the electrode surface area ratio that maximize and minimize the effect of the
sought-for parameters on the probe current are determined. The quantitative restrictions on the bias
potentials and the surface area ratio obtained in this study are used in the probe measurement
procedure and in the objective function for comparing the theoretical approximation of the probe
current with the measured I– characteristics.
A numerical simulation of probe measurements under the ionospheric conditions was conducted to verify
the efficiency of the procedure for extracting the local parameters of a four-component plasma from
the electron branch of the I –V characteristic of an isolated probe system. The results obtained may
be used in ionospheric plasma diagnostics onboard nanosatellites.
plasma ions of two species, isolated probe system with cylindrical electrodes,
mathematical model of current collection, parametric identification, a priori information
1. Boyd R. L. F. Langmuir probes on spacecraft, in Plasma Diagnostics. Lochte-Holtgreven (Ed.). Amsterdam: North-Holland Publ. Co., 1968. Pp. 732-776.
2. Chung, P. M., Talbot L., Touryan K. J. Electric Probes in Stationary and Flowing Plasmas. Springer-Verlag, 1975. 150 pp
https://doi.org/10.1007/978-3-642-65886-0
3. Online resource - https://ccmc.gsfc.nasa.gov/modelweb/models/iri2012_vitmo.php.
4. Lazuchenkov D. N., Lazuchenkov N. M. Interpretation of probe measurements in a collisionless plasma flow. Teh. Meh. 2018. No. 1. Pp. 107-120. (in Russian).
https://doi.org/10.15407/itm2018.01.107
5. Lazuchenkov D. N., Lazuchenkov N. M. Simulation of the extraction of the kinetic parameters of the ionospheric plasma from the current-voltage characteristics of a cylindrical probe. Teh. Meh. 2019. No. 4. Pp. 107-118. (in Russian).
https://doi.org/10.15407/itm2019.04.107
6. Lazuchenkov D. N., Lazuchenkov N. M. Determination of the parameters of a supersonic dissociated rarefied plasma flow from the current-voltage characteristics of an isolated system of cylindrical probes. Teh. Meh. 2020. No. 2. Pp. 80-88.
https://doi.org/10.15407/itm2020.02.080
7. Mott-Smith H., Langmuir I. The theory of collectors in gaseous discharges. Phys. Rev. 1926. V. 28. No. 5. Pp. 727-763.
https://doi.org/10.1103/PhysRev.28.727
8. Hoegy W. R., Wharton L. E., Current to a moving cylindrical electrostatic probe. Journal of Applied Physics. 1973. V. 44. No. 12. Pp. 5365-5371.
https://doi.org/10.1063/1.1662157
9. Laframboise J. G. Theory of Spherical and Cylindrical Langmuir Probes in a Collisionless Maxwellian Plasma at Rest. Report No. 100. Univ. of Toronto, Institute of Aerospace Studies. 1966. 210 pp.
https://doi.org/10.21236/AD0634596
10. Godard R., Laframboise J. Total current to cylindrical collectors in collisionless plasma flow. Space Science. 1983. V. 31, No. 3. Ðp. 275-283.
https://doi.org/10.1016/0032-0633(83)90077-6
Copyright (©) 2020 Lazuchenkov D. N., Lazuchenkov N. M.
Copyright © 2014-2020 Technical mechanics
____________________________________________________________________________________________________________________________
|
GUIDE FOR AUTHORS
====================
Open Access Policy
====================
REGULATIONS
on the ethics of publications
====================
|