Simulating of ion and electron trajectories in thermal plasma in electric field of a satellite by the molecular dynamic method
... Математическое моделирования обтекания тел потоками столкновительной и бесстолкновительной плазмы. М., 2010.
8. Katz I., Mandell M. L. Differential charging of high-voltage spacecraft: The equilibrium potential of insulated surfaces // J. Geophys. Res. 1982. Vol. 87. P. 5433.
9. Katz I., Stannart P. R., Gedeon L. et al. NASCAP simulations of spacecraft charging of the SCATHA satellite // Spacecraft/plasma interactions ...
A modeling the interaction of a oxygen plasma with a positively charged microsatellite with the molecular dynamics modeling method
... Geophys. 1998. Vol. 16. P. 1086—1096.
4. Hamelin M., Bouhram M., Dubouloz N. et al. Combined effects of satellite and ion detector geometries and potentials on the measurements of thermal ions. The Hyperboloid instrument on Interball // Proc. 7th Spacecraft Charging Technology Conference, 23—27 April 2001, ESTEC, Noordwijk, The Netherlands. ESA SP-476. P. 569—574.
5. Bouhram M., Dubouloz N., Hamelin M. et al. Electrostatic interaction between Interball-2 and the ambient plasma. 1. Determination ...
2D modeling of ion shadow behind a charged satellite by the method of molecular dynamics
... plasma were considered — 8 and 20 km s-1, respectively. It is shown that an increase in velocity and concentration of particles of ion shadow behind the satellite becomes more expressed.
1. Katz I., Mandell M. L. Differential charging of high-voltage spacecraft: The equilibrium potential of insulated surfaces // J. Geophys. Res. 1982. Vol. 87. P. 5433.
2. Katz I., Stannart P. R., Gedeon L. et al. NASCAP simulations of spacecraft charging of the SCATHA satellite // Spacecraft/plasma interactions and ...
Simulation of ion distribution near charged satellite by molecular dynamics simulation method. 2D approximation
... Langmuir sheath around Interball-2 // Ann. Geophys. 1998. Vol. 16. P. 1086—1096.
5. Bouhram M., Dubouloz N., Hamelin M. et al. Plasma sheath analysis and current calculations from the potential distribution around Interball Auroral probe // 2001:
A spacecraft charging odyssey. Proceeding of the 7th Spacecraft Charging Technology Conference, 2001, ESTEC, Noordwijk, The Netherlands. ESA SP-476. P. 557—561.
6. Hamelin M., Bouhram M., Dubouloz N. et al. Combined effects of satellite and ion detector ...
Modeling the formation of ion shadows behind a positively charged microsatellite in an oxygen plasma by the molecular dynamics method
... concentration is practically formed.
1. Hamelin M., Bouhram M., Dubouloz N. et al. Combined effects of satellite and ion detector geometries and potentials on the measurements of thermal ions. The Hyperboloid instrument on Interball // Proc. 7th Spacecraft Charging Technology Conference, 23—27 April 2001, ESTEC, Noordwijk, The Netherlands. ESA SP-476. P. 569—574.
2. Bouhram M., Dubouloz N., Hamelin M. et al. Electrostatic interaction between Interball-2 and the ambient plasma. 1. Determination ...
To the question of creating a stationary plasma engine of increased power
The new concept of powerful electric thrusters for spacecraft are aimed at creation of power plants for transportation of satellites with a large mass support manned space programs, space transportation and missions to study outer space. As the main engine for such systems, the choice of stationary plasma ...
Modeling of H Thermal Ions Measurements onboard Charged Satellite Taking into Account Anisotropy of Temperature
... potential increases these effects.
1.
Hamelin
M
.,
Bouhram
M
.,
Dubouloz
N
.
et
al
.
Combined effects of satellite and ion detector geometries and potentials on the measurements of thermal ions. The Hyperboloid instrument on Interball, in Proc. 7th Spacecraft Charging Technology Conference, 23—27 April 2001, ESTEC, Noordwijk, The Netherlands. ESA
SP
-476.
P
.
569—574.
2.
Зинин Л.
В., Гальперин Ю.
И., Григорьев С.
А. и др.
Об измерениях ...
The choice of structural materials for thermo thruster on clean monopropellant
... Annual AIAA/USU Conference of Small Satellites. SSC13-VII-2.
2. Spores R. A., Masse R., Kimbrel S., McLean C. GRIM AF-M315E Propulsion System // 49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. AIAA. P. 2013—3849.
3. Pokrupa N., Anflo K. Spacecraft system level design with regard to incorporation of a new green propulsion system // 47th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. AIAA. P. 2011—6129.
Goza D., Nesterenko A., Rumyantsev A.
low-thrust liquid rocket engine; ...
Using iodine gas as the working fluid for stationary plasma thrusters
The expediency of using iodine as the working fluid in the stationary plasma rocket engines is performed. The use of iodine is alternative for xenon, which due to a number of shortcomings can not be used in the engines of its high power for spacecraft.
1. C. Hillier A. C., Branam R. D., Huffman R. E. et al. Thrust Density Propellants in Hall Thrusters // AIAA 2011-5240. Florida, USA. 2011. P. 1—15.
2. Kieckhafer A., King L. B. Energetics of Propellant Options for High-Power Hall Thrusters ...
Investigation of discharge chamber insulator relative erosion of stationary plasma thruster
... Electric Propulsion Conference. Princeton, 2005. Р. 1—10.
2. Karabadzhak G. F., Semenkin A. V., Tverdokhlebov S. O. Semi-Empirical Method for Evaluation of a Xenon Operating Hall Thruster Erosion Rate Through Analysis of It`s Emission Spectra // Spacecraft Propulsion, Third International Conference European Space Agency ESASP-465. 2001. Р. 909.
3. Raitses Y., Staack D., Dorf L., Fisch N. J. Controlling Ion Acceleration Region in Hall thrusters // IEPC-2005—053, 29th International Electric ...
An algorithm and model of data saving for solving the problem of satellite-plasma interaction by the molecular dynamic method using the CUDA technology
... заряженном спутнике // Космические исследования. 1995. Т. 33, № 6. С. 563—571.
3. Bouhram M., Dubouloz N., Hamelin M. et al. Electrostatic interaction between In-terball-2 and the ambient plasma. 1. Determination of the spacecraft potential from current calculations // Ann. Geophys. 2002. Vol. 20, N 3. P. 365—376.
4. Hamelin M., Bouhram M., Dubouloz N. et al. Electrostatic interaction between In-terball-2 and the ambient plasma. 2. Influence on the low energy ion ...
Hall effect thrusters for small-sized spacecrafts
The results of investigation tests and comparative analysis of various low-power Electric Propulsion (EP) designed for their application as a part of electric propulsion systems (EPS) for small-sized spacecrafts are presented. Based on the analysis of main parameters and characteristics, the most prospective scheme of the EP design has been selected.
1. Potapenko M.Yu., Gopanchuk V. V. Characteristic Relationship between Dimensions and Parameters ...
Study of conditions of electric breakdown in the flow part of electrical insulators of electric propulsion propellant supply systems
The results of study of conditions of origination of electrical breakdown of gas in dielectric insulators of anode propellant (xenon) supply lines of prospective high-impulse increased-power electric thrusters intended for spacecraft orientation and stabilization are presented.
1.
Райзер Ю.
П.
Физика газового разряда: учеб. руководство. М
., 1987.
2.
Kozubsky K., Kudriavtsev S.
et al. Study of Gas-Electrical Terminal ...