Numerical modeling of spacecraft electric propulsion thrusters
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[1] Monika Auweter-Kurtz,et al. Experimental and numerical investigation of a power augmented thermal arc jet , 2001 .
[2] Gregory G. Spanjers,et al. Electromagnetic Effects in the Near Field Plume Exhaust of a Micro-Pulsed-Plasma Thruster , 2002 .
[3] M. Martinez-Sanchez,et al. Two-fluid nonequilibrium simulation of hydrogen arcjet thrusters , 1996 .
[4] G. Butler,et al. Single and two fluid simulations of arcjet performance , 1992 .
[5] Andrey A. Shagayda,et al. Fully Kinetic Modeling of Low-Power Hall Thrusters , 2005 .
[6] L. Garrigues,et al. Low frequency oscillations in a stationary plasma thruster , 1998 .
[7] M. Keidar,et al. On the magnetic mirror effect in Hall thrusters , 2005 .
[8] Ian Coxhill,et al. A Xenon Resistojet Propulsion System for Microsatellites , 2005 .
[9] L. Garrigues,et al. Modeling of double stage Hall effect thruster , 2005, IEEE Transactions on Plasma Science.
[10] Charles K. Birdsall,et al. Particle-in-cell charged-particle simulations, plus Monte Carlo collisions with neutral atoms, PIC-MCC , 1991 .
[11] L. Garrigues,et al. Model study of the influence of the magnetic field configuration on the performance and lifetime of a Hall thruster , 2003 .
[12] V. Kim. Main Physical Features and Processes Determining the Performance of Stationary Plasma Thrusters , 1998 .
[13] Rodney L. Burton,et al. Plasmadynamics model for nonequilibrium processes in N2/H2 arcjets , 1995 .
[14] Michael Keidar,et al. Vaporization of heated materials into discharge plasmas , 2001 .
[15] L. Garrigues,et al. Two-dimensional model of a stationary plasma thruster , 2002 .
[16] James E. Polk,et al. Theoretical model of a hollow cathode plasma for the assessment of insert and keeper lifetimes , 2005 .
[17] C. Fletcher. Computational techniques for fluid dynamics , 1992 .
[18] Eduardo Ahedo,et al. A model of the two-stage Hall thruster discharge , 2005 .
[19] Iain D. Boyd,et al. Computational model of a Hall thruster , 2004, Comput. Phys. Commun..
[20] J. Adam,et al. Study of stationary plasma thrusters using two-dimensional fully kinetic simulations , 2004 .
[21] Pierre Degond,et al. Numerical simulation of electron transport in the channel region of a stationary plasma thruster , 2002 .
[22] M. Keidar,et al. A Hydrodynamic-Based Erosion Model for Hall Thrusters , 2005 .
[23] M. Keidar,et al. Modeling of a high-power thruster with anode layer , 2004 .
[24] Monika Auweter-Kurtz,et al. High-Power Hydrogen Arcjet Thrusters , 1998 .
[25] James E. Polk,et al. Three-Dimensional Particle Simulations of Ion-Optics Plasma Flow and Grid Erosion , 2003 .
[26] L. Garrigues,et al. Critical assessment of a two-dimensional hybrid Hall thruster model: Comparisons with experiments , 2004 .
[27] Manuel Martinez-Sanchez,et al. A COMPUTATIONAL STUDY OF INTERNAL PHYSICAL EFFECTS IN A HALL THRUSTER , 2002 .
[28] R. E. Peterkin,et al. Transport of Magnetic Flux in an Arbitrary Coordinate ALE Code , 1998 .
[29] Robert Alexander Bond,et al. Ion thruster extraction grid design and erosion modelling using computer simulation , 1995 .
[30] M. Keidar,et al. Plasma flow and plasma–wall transition in Hall thruster channel , 2001 .
[31] John Michael Fife,et al. Two-dimensional hybrid particle-in-cell modeling of Hall thrusters , 1995 .
[32] H. Dan Thomas,et al. A NUMERICAL STUDY OF A PULSED PLASMA THRUSTER , 2001 .
[33] Monika Auweter-Kurtz,et al. 1 kW Ammonia Arcjet System Development for a Science Mission to the Moon , 2005 .
[34] Thomas Stueber,et al. Discharge Chamber Primary Electron Modeling Activities in 3-Dimension , 2004 .
[35] Pavlos Mikellides,et al. Pulsed Plasma Thrusters for Microsatellite Propulsion: Techniques for Optimization , 2000 .
[36] Iain D. Boyd,et al. Monte Carlo simulation of nonequilibrium flow in a low-power hydrogen arcjet , 1997 .
[37] Iain D. Boyd,et al. Monte Carlo simulation of nonequilibrium flow in low power hydrogen arcjets , 1996 .
[38] Iain D. Boyd,et al. Modeling the plasma plume of a hollow cathode , 2004 .
[39] Iain D. Boyd,et al. Experimental and numerical investigations of low-density nozzle and plume flows of nitrogen , 1992 .
[40] Dennis Keefer,et al. Plasma particle simulation of electrostatic ion thrusters , 1992 .
[41] L. Garrigues,et al. Computation of Hall Thruster Performance , 2001 .
[42] Pavlos Mikellides,et al. Modeling of ablation-fed pulsed plasma thrusters , 1995 .
[43] Iain D. Boyd,et al. Computational and experimental investigations of rarefied flows in small nozzles , 1996 .
[44] Yevgeny Raitses,et al. Hall thruster with absorbing electrodes , 2000 .
[45] Iain Boyd,et al. GRID EROSION ANALYSIS OF THE T5 ION THRUSTER , 2001 .
[46] M. Keidar,et al. Electrical Discharge in the Teflon Cavity of a Coaxial , 2000 .
[47] G. Bird. Molecular Gas Dynamics and the Direct Simulation of Gas Flows , 1994 .
[48] C. Birdsall,et al. Plasma Physics via Computer Simulation , 2018 .
[49] H. D. Thomas,et al. Numerical modeling of a pulsed plasma thruster , 2001 .
[50] R. Pletcher,et al. Computational Fluid Mechanics and Heat Transfer. By D. A ANDERSON, J. C. TANNEHILL and R. H. PLETCHER. Hemisphere, 1984. 599 pp. $39.95. , 1986, Journal of Fluid Mechanics.
[51] Suk C. Kim. Calculations of low-Reynolds-number resistojet nozzles , 1994 .
[52] Andrew D. Ketsdever,et al. Predicted Performance and Systems Analysis of the Free Molecule Micro-Resistojet , 2000 .
[53] D. Murray,et al. Numerical modelling of ion thruster hollow cathode interior flow , 1997 .
[54] S. Aso,et al. Numerical Studies on Effect of Nozzle Geometry and of Flow Continuity on Thrust Performance , 2001 .
[55] K. Komurasaki,et al. Two-dimensional numerical model of plasma flow in a Hall thruster , 1995 .
[56] Thomas J. Stueber. Ion Thruster Discharge Chamber Simulation in Three Dimension , 2005 .
[57] James E. Polk,et al. One-Dimensional Hollow Cathode Model , 2003 .
[58] Gregory G. Spanjers,et al. Propellant charring in pulsed plasma thrusters , 2004 .
[59] Iain D. Boyd,et al. Extensive Validation of a Monte Carlo Model for Hydrogen Arcjet Flowfields , 1997 .
[60] P. Turchi,et al. Pulsed Plasma Thruster , 1998 .
[61] David Nicolini,et al. The Design, Development and in-flight Operation of a Water Resistojet Micropropulsion System , 2004 .
[62] M. Jugroot. Numerical Modeling of Neutral and Charged Particles within a Gridded Ion Thruster , 2001 .
[63] M. Martínez-Sánchez,et al. A numerical study of low-frequency discharge oscillations in Hall thrusters , 1997 .
[64] Andrew D. Ketsdever,et al. Micropropulsion for small spacecraft , 2000 .
[65] E. Ahedo,et al. Partial trapping of secondary-electron emission in a Hall thruster plasma , 2005 .
[66] E. Ahedo,et al. One-dimensional model of the plasma flow in a Hall thruster , 2001 .
[67] R. Wirz,et al. 2-D Discharge Chamber Model for Ion Thrusters , 2004 .
[68] Michael Keidar,et al. Model of an electrothermal pulsed plasma thruster , 2003 .
[69] Paul J. Wilbur,et al. Numerical simulation of ion beam optics for many-grid systems , 2001 .
[70] James Szabo,et al. Fully Kinetic Hall Thruster Modeling IEPC-01-341 , 2001 .