
Thermal calculation of the anode of the stationary plasma engine
... erosion, beam and plasma characterisation of a SPT100D EM1 with an advanced electric propulsion diagnostic system // IEPS2009141, 31st International Electric Propulsion Conferense. Michigan, 2009.
Chubov P., Rumyantsev A., Kharjukov V.
Stationary Plasma Thruster, thermal calculation, anode gas distributor, stationary mode, dynamic mode
4450

Modeling of the cathode thermal conditions
This article provides results of the cathode of stationary plasma engine thermal vacuum test with various operating modes simulated, a thermal calculation and the cathode thermal mathematical model verification. Based on the calculations, the cathode thermal model and operating performances were assessed, the most efficient ...

A modeling the interaction of a oxygen plasma with a positively charged microsatellite with the molecular dynamics modeling method
... ионов тепловой плазмы в электрическом поле спутника методом молекулярной динамики // Там же. 2014. № 10. С. 47—52.
Zinin L., Sharamet A, Vasileva A.
mathematical modeling, thermal plasma, molecular dynamics method, charged satellite
2934

Modeling the formation of ion shadows behind a positively charged microsatellite in an oxygen plasma by the molecular dynamics method
... Балтийского федерального университета им. И. Канта. Сер.: Физикоматематические и технические науки. 2017. № 2. С. 29—34.
Zinin L., Sharamet A., Vasileva A.
mathematical modeling, thermal plasma, molecular dynamics method, charged satellite, ion shadow
4852

Modeling of H Thermal Ions Measurements onboard Charged Satellite Taking into Account Anisotropy of Temperature
... «Современные проблемы прикладной математики и математического моделирования», 2—7 февраля 2009 г. Ч. 2. Воронеж, 2009.
C
. 59—61.
Zinin L. V.
ionosphere, thermal plasma, massspectrometer, measurement simulation.
5663
10.5922/222320952009104

Simulating of ion and electron trajectories in thermal plasma in electric field of a satellite by the molecular dynamic method
A threedimensional model of the interaction of a charged micro satellite and thermal plasma was considered. The ion and electron trajectories for different initial velocities and directions are shown. The calculated particle trajectories have some deviations from the classical trajectories in crossed electric and magnetic fields. The ...

Nonstationary polar wind in presence of magnetosphere convection
... hydrodynamic model TUBE 7 is used for modeling of fieldaligned motions and temperature of polar ionosphere ions taking into account magnetosphere convection. It was shown tube geometry changing have a great influence on basic parameters of polar magnetosphere thermal plasma.
1.
Banks P. M., Holzer
Т
.
Е
.
The polar wind // J. Geophys. Res. 1968. Vol. 73, №
21. P. 6846—6854.
2.
Banks P. M., Holzer
Т
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Е
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Features of plasma transport in the upper atmosphere // J. Geophys. Res. 1969. Vol....

2D modeling of ion shadow behind a charged satellite by the method of molecular dynamics
It was considered a twodimensional model of the interaction of a charged micro satellite and thermal plasma. The method of molecular dynamics used as a modeling method. Ion concentration distributions near SC were calculated for 10 and 102 protons in cm2 and the two values of relative satellite velocity and plasma were considered — 8 and 20 km s1,...

Simulation of ion distribution near charged satellite by molecular dynamics simulation method. 2D approximation
Mathematical model of interaction between low density thermal plasma with charged simple shape space probe was considered. Molecular dynamics simulation method was used. Modeling result shows a positive cloud of protons before the satellite and ion shadow behind it.
1. Гальпеpин Ю. И., Гpигоpьев ...

An algorithm and model of data saving for solving the problem of satelliteplasma interaction by the molecular dynamic method using the CUDA technology
This article considers a parallel algorithm of the mathematical model of interaction between a charged small satellite and thermal space plasma. The main problem of the algorithm implementation is to maintain the total amount of current data for each calculator and to synchronize and minimize exchanges. The range of graphics accelerators chosen for calculation makes it possible to focus ...

Creation of the effective cathode jack for the microSPD
... О. А., Муравьев В. А., Шагайда А. А. Холловские и ионные плазменные двигатели для космических аппаратов. М., 2008.
Katashova M., Parakhin G., Rumyantsev A.
stationary plasma thruster (SPT), microSPT, cathodecompensator, thermal emission, scandium barian cathode, screen vacuum heartinsulation
2932