Computational simulation of Faraday probe measurements

[1]  William L. Briggs,et al.  A multigrid tutorial , 1987 .

[2]  W. Steckelmacher.  Molecular gas dynamics and the direct simulation of gas flows , 1996 .

[3]  I. Langmuir.  The Interaction of Electron and Positive Ion Space Charges in Cathode Sheaths , 1929 .

[4]  Randy Aadland,et al.  BPT Hall thruster plume characteristics , 1999 .

[5]  G. Manfredi,et al.  Kinetic simulations of ion temperature measurements from retarding field analyzers , 2002 .

[6]  Mark A. Cappelli,et al.  Wall Erosion in 2D Hall Thruster Simulations , 2006 .

[7]  James E. Polk,et al.  Analysis of Plume Backflow From a Lithium Magnetoplasmadynamic Thruster , 2005 .

[8]  C. Birdsall,et al.  Plasma Physics via Computer Simulation , 2018 .

[9]  J. Peraire,et al.  Hybrid-PIC Simulation of a Hall Thruster Plume on an Unstructured Grid with DSMC Collisions , 2003 .

[10]  Alec D. Gallimore,et al.  Near- and Far-Field Characterization of Stationary Plasma Thruster Plumes , 2001 .

[11]  Alec D. Gallimore,et al.  Effect of Backpressure on Ion Current Density Measurements in Hall Thruster Plumes , 2005 .

[12]  J. Sanderson,et al.  The Physics of Plasmas: Index , 2003 .

[13]  Chung,et al.  Kinetic theory of ion collection by probing objects in flowing strongly magnetized plasmas. , 1988, Physical review. A, General physics.

[14]  M. Cappelli,et al.  Experimental Characterization of a Micro-Hall Thruster , 2007 .

[15]  J. N. Davidson,et al.  Electric sheath and presheath in a collisionless, finite ion temperature plasma , 1980 .

[16]  Eric J. Pencil,et al.  Triple Langmuir probe measurements in the plume of a pulsed plasma thruster , 1998 .

[17]  Alec D. Gallimore,et al.  Magnetically filtered Faraday probe for measuring the ion current density profile of a Hall thruster , 2006 .

[18]  G. Fairweather,et al.  Some high accuracy difference schemes with a splitting operator for equations of parabolic and elliptic type , 1967 .

[19]  R. S. Robinson,et al.  Physics of closed drift thrusters , 1999 .

[20]  Mariano Andrenucci,et al.  Qualification Status of the FEEP-150 Electric Micropropulsion Subsystem , 2005 .

[21]  James R. Wertz,et al.  Space Mission Analysis and Design , 1992 .

[22]  Eric Pencil,et al.  Far-field plume contamination and sputtering of the stationary plasma thruster , 1994 .

[23]  N. Hershkowitz,et al.  Ion flow and sheath physics studies in multiple ion species plasmas using diode laser based laser-induced fluorescence , 2006 .

[24]  R. K. Wakerling,et al.  The characteristics of electrical discharges in magnetic fields , 1949 .

[25]  Lee S. Mason,et al.  Spacecraft Interaction Test Results of the High Performance Hall System SPT-140 (Postprint) , 2000 .

[26]  A. Bers,et al.  Waves in anisotropic plasmas , 1963 .

[27]  M. Mitchner,et al.  Partially ionized gases , 1973 .

[28]  M. Keidar,et al.  Calculation of Boron Nitride Sputter Yields Under Low Energy Xenon Ion Bombardment , 2007 .

[29]  K. Riemann,et al.  Kinetic theory of the plasma sheath transition in a weakly ionized plasma , 1981 .

[30]  Michael Keidar,et al.  An Investigation of Factors Involved in Hall Thruster Wall Erosion Modeling , 2006 .

[31]  T. Teichmann,et al.  Introduction to physical gas dynamics , 1965 .

[32]  Iain D. Boyd,et al.  Modeling of the near field plume of a Hall thruster , 2004 .

[33]  D. Fedosov,et al.  Transient heat transfer and gas flow in a MEMS-based thruster , 2006, Journal of Microelectromechanical Systems.

[34]  Francis F. Chen,et al.  Introduction to Plasma Sources , 2003 .

[35]  Iain D. Boyd,et al.  3D Simulation of Plume Flows from a Cluster of Plasma Thrusters , 2005 .

[36]  Octavio Camino,et al.  SMART-1 Electric Propulsion Operations , 2004 .

[37]  William Hargus,et al.  The Air Force Clustered Hall Thruster Program , 2002 .

[38]  A. Gallimore,et al.  A High-Speed Probe Positioning System for Interrogating the Discharge Plasma of a 30 cm Ion Thruster , 2002 .

[39]  J. G. Laframboise.  Theory of spherical and cylindrical Langmuir probes in a collisionless , 1966 .

[40]  K. Chung,et al.  Effects of a generalized presheath source in flowing magnetized plasmas , 1991 .

[41]  Thomas E. Schwartzentruber,et al.  A modular particle-continuum numerical method for hypersonic non-equilibrium gas flows , 2007, J. Comput. Phys..

[42]  Alec D. Gallimore,et al.  THE EFFECTS OF CLUSTERING MULTIPLE HALL THRUSTERS ON PLASMA PLUME PROPERTIES , 2003 .

[43]  Edgar Y. Choueiri,et al.  MEMS Mega-pixel Micro-thruster Arrays for Small Satellite Stationkeeping , 2000 .

[44]  Hutchinson,et al.  Ion collection by probes in strong magnetic fields with plasma flow. , 1987, Physical review. A, General physics.

[45]  P. Wesseling.  An Introduction to Multigrid Methods , 1992 .

[46]  Effect of a Magnetic Field in Simulating the Very Near-Field Plume of an Anode Layer Hall Thruster , 2007 .

[47]  Robert S. Jankovsky,et al.  Laboratory Model 50 kW Hall Thruster , 2002 .

[48]  A. Lichtenberg,et al.  Principles of Plasma Discharges and Materials Processing , 1994 .

[49]  William H. Press,et al.  Numerical recipes in Fortran 90: the art of parallel scientific computing, 2nd Edition , 1996, Fortran numerical recipes.

[50]  R. Jahn,et al.  Physics of Electric Propulsion , 1968 .

[51]  I. Hutchinson.  Principles of Plasma Diagnostics , 1987 .

[52]  Alec D. Gallimore,et al.  Preliminary Plume Characterization of a Low-Power Hall Thruster Cluster , 2002 .

[53]  Daniel E. Hastings,et al.  Modeling of Stationary Plasma Thruster-100 Thruster Plumes and Implications for Satellite Design , 1999 .

[54]  Douglas C. Giancoli,et al.  Physics for scientists and engineers with modern physics (4th edition) , 2008 .

[55]  John R. Brophy,et al.  Cyclic Endurance Test of an SPT-100 Stationary Plasma Thruster , 1994 .

[56]  I. Kaganovich.  How to patch active plasma and collisionless sheath: A practical guide , 2002, physics/0208041.

[57]  Alec D. Gallimore,et al.  Ion species fractions in the far-field plume of a high-specific impulse Hall thruster , 2003 .

[58]  R. Dressler,et al.  Ion Dynamics in Hall Effect and Ion Thrusters: Xe' + Xe Symmetric Charge , 2000 .

[59]  M. P. Levin,et al.  Numerical Recipes In Fortran 90: The Art Of Parallel Scientific Computing , 1998, IEEE Concurrency.

[60]  Bruce A. Banks,et al.  Sputtering Erosion Measurement on Boron Nitride as a Hall Thruster Material , 2002 .

[61]  Michael Keidar,et al.  PLASMA DENSITY REDUCTION USING ELECTROMAGNETIC E×B FIELD DURING REENTRY FLIGHT , 2007 .

[62]  Edgar Y. Choueiri,et al.  A Critical History of Electric Propulsion: The First 50 Years (1906-1956) , 2004 .

[63]  J. E. Polk,et al.  NSTAR Xenon Ion Thruster on Deep Space 1: Ground and flight tests (invited) , 2000 .

[64]  M. Keidar,et al.  Particle Simulations of a Hall Thruster Plume , 2000 .

[65]  H. H. Rachford,et al.  The Numerical Solution of Parabolic and Elliptic Differential Equations , 1955 .

[66]  N. Hershkowitz,et al.  Experimental studies of the Bohm criterion in a two-ion-species plasma using laser-induced fluorescence. , 2003, Physical review letters.

[67]  M. Keidar,et al.  Transition from plasma to space-charge sheath near the electrode in electrical discharges , 2004, IEEE Transactions on Plasma Science.

[68]  R. McEachran,et al.  Relativistic low-energy elastic and momentum transfer cross sections for electron scattering from xenon , 1987 .

[69]  K. Riemann.  Plasma-sheath transition in the kinetic tonks-langmuir model , 2006 .

[70]  T. Gombosi.  Gaskinetic Theory: Shock Waves , 1994 .

[71]  Jared M. Ekholm,et al.  E x B Measurements of a 200 W Xenon Hall Thruster , 2005 .

[72]  Alec D. Gallimore,et al.  Transport-Property Measurements in the Plume of an SPT-100 Hall Thruster , 1998 .

[73]  H. Kuninaka,et al.  Assessment of Plasma Interactions and Flight Status of the HAYABUSA Asteroid Explorer Propelled by Microwave Discharge Ion Engines , 2006, IEEE Transactions on Plasma Science.

[74]  T. Randolph,et al.  End-of-life Stationary Plasma Thruster far-field plume characterization , 1996 .

[75]  Alec D. Gallimore,et al.  The Performance and Plume Characterization of a Laboratory Gridless Ion Thruster with Closed Electron Drift Acceleration , 2004 .