Electric propulsion for satellites and spacecraft: established technologies and novel approaches
暂无分享,去创建一个
[1] Keith A. McFall,et al. Investigation of propellant inefficiencies in a pulsed plasma thruster , 1996 .
[2] LIQUID PROPELLANT PULSED PLASMA THRUSTER , 2003 .
[3] Dan M. Goebel,et al. Magnetic shielding of walls from the unmagnetized ion beam in a Hall thruster , 2013 .
[4] C. Charles,et al. Volume and surface propellant heating in an electrothermal radio-frequency plasma micro-thruster , 2014 .
[5] C. Charles,et al. A supersonic ion beam generated by a current-free helicon double-layer , 2003 .
[6] J. Jarrige,et al. Characterization of a coaxial ECR plasma thruster , 2013 .
[7] S. Tsikata,et al. Three-dimensional structure of electron density fluctuations in the Hall thruster plasma: E¯×B¯ mode , 2010 .
[8] J. Adam,et al. High-frequency electron drift instability in the cross-field configuration of Hall thrusters , 2006 .
[9] A. Lichtenberg,et al. Principles of Plasma Discharges and Materials Processing , 1994 .
[10] M. Lieberman,et al. Global model of Ar, O2, Cl2, and Ar/O2 high‐density plasma discharges , 1995 .
[11] S. Mazouffre. Laser-induced fluorescence diagnostics of the cross-field discharge of Hall thrusters , 2012 .
[12] E. Ahedo,et al. Combined effects of electron partial thermalization and secondary emission in Hall thruster discharges , 2007 .
[13] N. Fisch,et al. Cross-field electron transport induced by a rotating spoke in a cylindrical Hall thruster , 2012 .
[14] Michael J. Patterson,et al. High Thrust-to-Power Annular Engine Technology , 2015 .
[15] J. Sercel. Electron-cyclotron-resonance (ECR) plasma acceleration , 1987 .
[16] M. Merino,et al. Influence of Electron and Ion Thermodynamics on the Magnetic Nozzle Plasma Expansion , 2015, IEEE Transactions on Plasma Science.
[17] Boris N. Breizman,et al. Theoretical components of the VASIMR plasma propulsion concept , 2004 .
[18] K. Dannenmayer,et al. Ionization and acceleration processes in a small, variable channel width, permanent-magnet Hall thruster , 2012 .
[19] E. B. Hooper,et al. Plasma detachment from a magnetic nozzle , 1991 .
[20] John W. Dankanich,et al. Low-thrust Propulsion Technologies, Mission Design, and Application , 2010 .
[21] S. Mazouffre,et al. Observation of high-frequency ion instabilities in a cross-field plasma , 2015 .
[22] A. Aanesland,et al. Global model of a gridded-ion thruster powered by a radiofrequency inductive coil , 2012 .
[24] Edgar Y. Choueiri,et al. A Critical History of Electric Propulsion: The First 50 Years (1906-1956) , 2004 .
[25] Christine Charles,et al. Investigation of radiofrequency plasma sources for space travel , 2012 .
[26] M. Keidar,et al. Modeling of a high-power thruster with anode layer , 2004 .
[27] Vaios Lappas,et al. Direct thrust measurement of a permanent magnet helicon double layer thruster , 2011 .
[28] W. Choe,et al. Effect of magnetic field configuration on the multiply charged ion and plume characteristics in Hall thruster plasmas , 2015 .
[29] S. Mazouffre,et al. Elementary Scaling Relations for Hall Effect Thrusters , 2011 .
[30] J. Jarrige,et al. Performance Comparison of an ECR Plasma Thruster using Argon and Xenon as Propellant Gas , 2013 .
[31] Francis F. Chen,et al. Helicons-the early years , 1997 .
[32] Michael D. West,et al. Testing a Helicon Double Layer Thruster Immersed in a Space-Simulation Chamber , 2008 .
[33] Günter Dr. Kornfeld,et al. Physics and Evolution of HEMP-Thrusters , 2007 .
[34] Mark A. Cappelli,et al. Ion Velocity and Plasma Potential Measurements of a Cylindrical Cusped Field Thruster , 2012 .
[35] Michael Keidar,et al. The VHITAL Program to Demonstrate the Performance and Lifetime of a Bismuth-Fueled Very High Isp Hall Thruster , 2005 .
[36] K. Nishiyama,et al. Powered Flight of Electron Cyclotron Resonance Ion Engines on Hayabusa Explorer , 2007 .
[37] Arnold J. Kelly,et al. Mass savings domain of plasma propulsion for LEO to GEO transfer , 1993 .
[38] A. M. Pichitino. Rocket propulsion elements: by George P. Sutton. 294 pages, 14 × 22 cm., illustrations, plates. New York, John Wiley & Sons, Inc., 1949. Price, $4.50 , 1949 .
[39] A. Fruchtman. Energizing and depletion of neutrals by a collisional plasma , 2008 .
[40] Robert S. Jankovsky,et al. A Hall Thruster Performance Model Incorporating the Effects of a Multiply-Charged Plasma , 2001 .
[41] Lee S. Mason,et al. Development of NASA's Small Fission Power System for Science and Human Exploration , 2015 .
[42] A. Sasoh,et al. Technology and Application Aspects of Applied Field Magnetoplasmadynamic Propulsion , 1998 .
[43] Pascal Chabert,et al. Space Exploration Technologies Pegases A new promising electric propulsion concept , 2011 .
[44] N. Hershkowitz,et al. Ambipolar ion acceleration in an expanding magnetic nozzle , 2011 .
[45] R. Welle. Space propulsion applications of helium arcjets , 1997 .
[46] Denis Packan,et al. Optimization of a coaxial electron cyclotron resonance plasma thruster with an analytical model , 2015 .
[47] V. Godyak,et al. Electron energy distribution function and plasma parameters across magnetic filters , 2012 .
[48] Kyoichi Kuriki,et al. Transitional Behavior of MPD Arcjet Operation , 1978 .
[49] Christine Charles,et al. Current-free double-layer formation in a high-density helicon discharge , 2003 .
[50] I. Mikellides,et al. Magnetic shielding of a laboratory Hall thruster. II. Experiments , 2014 .
[51] Paul McNamara,et al. The LISA Pathfinder Mission , 2010 .
[52] J. Adam,et al. Anomalous conductivity in Hall thrusters: Effects of the non-linear coupling of the electron-cyclotron drift instability with secondary electron emission of the walls , 2013 .
[53] M. Merino,et al. Plasma detachment in a propulsive magnetic nozzle via ion demagnetization , 2014 .
[54] J. Jarrige,et al. Experimental geometry investigation of a coaxial ECR plasma thruster , 2015 .
[55] Michael R. LaPointe,et al. High Power MPD Thruster Performance Measurements , 2004 .
[56] R. S. Robinson,et al. Physics of closed drift thrusters , 1999 .
[57] F. C. Díaz. The VASIMR Rocket. , 2000 .
[58] E. Ahedo. Double-layer formation and propulsive assessment for a three-species plasma expanding in a magnetic nozzle , 2011 .
[59] Lee S. Mason,et al. Kilopower, NASA's Small Fission Power System for Science and Human Exploration , 2014 .
[60] David H. Manzella,et al. Investigation of the Erosion Characteristics of a Laboratory Hall Thruster , 2003 .
[61] A. Rezaeiha,et al. Review of Worldwide Activities in Liquid-Fed Pulsed Plasma Thruster , 2014 .
[62] Michael J. Patterson,et al. Near-Term High Power Ion Propulsion Options for Earth- Orbital Applications , 2009 .
[63] P. Turchi,et al. Pulsed Plasma Thruster , 1998 .
[64] L. Garrigues,et al. Model analysis of a double-stage Hall effect thruster with double-peaked magnetic field and intermediate electrode , 2007 .
[65] P. Rossetti,et al. Performance of an Applied Field MPD Thruster , 2001 .
[66] James E. Polk,et al. Implementation and Initial Validation of a 100-Kilowatt Class Nested-Channel Hall Thruster , 2014 .
[67] Paul A. Abell,et al. The Asteroid Redirect Mission and sustainable human exploration , 2015 .
[68] Mitchell L. R. Walker,et al. Ion production cost of a gridded helicon ion thruster , 2013 .
[69] James E. Polk,et al. Implementation and Initial Validation of a 100-kW Class Nested-channel Hall Thruster , 2014 .
[70] C. L. Dailey,et al. Large inductive thruster performance measurement , 1981 .
[71] A. Morozov,et al. Fundamentals of Stationary Plasma Thruster Theory , 2000 .
[72] C. Charles,et al. Performance characterization of a helicon double layer thruster using direct thrust measurements , 2011 .
[73] Dominique Harribey,et al. Visual Evidence of Magnetic Shielding With the PPS-Flex Hall Thruster , 2014, IEEE Transactions on Plasma Science.
[74] Kenichi Kubota,et al. Numerical Investigation of Ionization and Acceleration Processed in a Self-Field MPD Thruster , 2005 .
[75] E. Ahedo,et al. Low-frequency model of breathing oscillations in Hall discharges. , 2009, Physical review. E, Statistical, nonlinear, and soft matter physics.
[76] Dario Izzo,et al. Very high delta-V missions to the edge of the solar system and beyond enabled by the dual-stage 4-grid ion thruster concept , 2006 .
[77] H. Loeb. Plasma-based ion beam sources , 2005 .
[78] Paul J. Wilbur,et al. Ion Thruster Development Trends and Status in the United States , 1998 .
[79] Dominique Harribey,et al. Optimization of a wall-less Hall thruster , 2015 .
[80] Eduardo Ahedo,et al. A model of the two-stage Hall thruster discharge , 2005 .
[81] G. Janes,et al. Anomalous Electron Diffusion and Ion Acceleration in a Low‐Density Plasma , 1966 .
[82] Manuel Martinez-Sanchez,et al. Experimentally Characterizing the Plume of a Divergent Cusped-Field Thruster , 2009 .
[83] K. Dannenmayer,et al. Examination of plasma-wall interactions in Hall effect thrusters by means of calibrated thermal imaging , 2007 .
[84] E. Choueiri. Fundamental difference between the two Hall thruster variants , 2001 .
[85] I. Mikellides,et al. Magnetic shielding of a laboratory Hall thruster. I. Theory and validation , 2014 .
[86] N. Fisch,et al. Electron-wall Interaction in Hall Thrusters , 2005 .
[87] Mitchell L. R. Walker,et al. A review of research in low earth orbit propellant collection , 2015 .
[88] E. Ahedo,et al. Effects of the radial plasma-wall interaction on the Hall thruster discharge , 2003 .
[89] David Y. Oh. Evaluation of Solar Electric Propulsion Technologies for Discovery Class Missions , 2007 .
[90] A. Fruchtman,et al. Electric field in a double layer and the imparted momentum. , 2006, Physical review letters.
[91] F. C. Díaz. An overview of the VASIMR engine: High power space propulsion with RF plasma generation and heating , 2002 .
[92] I. Mikellides,et al. Magnetic shielding of Hall thrusters at high discharge voltages , 2014 .
[93] V. Kim. Main Physical Features and Processes Determining the Performance of Stationary Plasma Thrusters , 1998 .
[94] Gregory A. Jerman,et al. Propulsion System Development for the Iodine Satellite (iSAT) Demonstration Mission , 2015 .
[95] M. Walker,et al. Thrust Measurements of a Helicon Plasma Source , 2011 .
[96] Samudra E. Haque,et al. Electric propulsion for small satellites , 2014 .
[97] L. Garrigues,et al. Anomalous conductivity and secondary electron emission in Hall effect thrusters , 2006 .
[98] Daniel G. Courtney,et al. Diverging Cusped-Field Hall Thruster ( DCHT ) IEPC-2007-39 , 2007 .
[99] A. Aanesland,et al. E × B probe measurements in molecular and electronegative plasmas. , 2015, The Review of scientific instruments.
[100] Edgar Y. Choueiri,et al. Scaling laws for electromagnetic pulsed plasma thrusters , 2001 .
[101] Michael Keidar,et al. Magnetically enhanced vacuum arc thruster , 2005 .
[102] Brian E. Beal,et al. Plasma Properties in the Plume of a Hall Thruster Cluster , 2004 .
[103] Eduardo Ahedo,et al. Presheath/sheath model with secondary electron emission from two parallel walls , 2002 .
[104] Dmytro Rafalskyi,et al. Experimental validation of the dual positive and negative ion beam acceleration in the plasma propulsion with electronegative gases thruster , 2014 .
[105] James Szabo,et al. High Density Hall Thruster Propellant Investigations , 2012 .
[106] W. Choe,et al. Radial scale effect on the performance of low-power cylindrical Hall plasma thrusters , 2013 .
[107] Artem Smirnov,et al. Enhanced ionization in the cylindrical Hall thruster , 2002 .
[108] P. Schreiner,et al. In Search of Alternative Propellants for Ion Thrusters IEPC-2015-320 / ISTS-2015-b-320 , 2015 .
[109] N. Meezan,et al. Anomalous electron mobility in a coaxial Hall discharge plasma. , 2000, Physical review. E, Statistical, nonlinear, and soft matter physics.
[110] E. Ahedo. Plasmas for space propulsion , 2011 .
[111] Francis M. Curran,et al. Extended life and performance test of a low-power arcjet , 1992 .
[112] Pascal Chabert,et al. Physics of radio-frequency plasmas , 2011 .
[113] M. Walker,et al. Effect of secondary electron emission on the plasma sheath , 2015 .
[114] C. L. Dailey,et al. Large inductive thruster performance measurement , 1981 .
[115] Adam Boxberger,et al. Experimental Investigation of Steady-State Applied-Field Magnetoplasmadynamic Thrusters at Institute of Space Systems , 2012 .
[116] Manuel Martinez-Sanchez,et al. Hybrid Particle-in-Cell Erosion Modeling of Two Hall Thrusters , 2008 .
[117] A. Gallimore,et al. Measurement of Cross-Field Electron Current in a Hall Thruster Due to Rotating Spoke Instabilities , 2011 .
[118] Andrea Kodys,et al. A Critical Review of the State-of-the-Art in the Performance of Applied-field Magnetoplasmadynamic Thrusters , 2005 .
[119] Joachim V. R. Heberlein,et al. New approaches in thermal plasma technology , 2002 .
[120] A. Anders,et al. A Theoretical Analysis of Vacuum Arc Thruster and Vacuum Arc Ion Thruster Performance , 2008, IEEE Transactions on Plasma Science.
[121] K. Dannenmayer,et al. Impact of discharge voltage on wall-losses in a Hall thruster , 2011 .
[122] Maxwell G. Ballenger,et al. Investigation of Plasma Detachment From a Magnetic Nozzle in the Plume of the VX-200 Magnetoplasma Thruster , 2015, IEEE Transactions on Plasma Science.
[123] Hideyuki Horisawa,et al. Very low-power arcjet testing , 2000 .
[124] C. Charles,et al. Performance improvement of a permanent magnet helicon plasma thruster , 2013 .
[126] N. Hershkowitz. Review of recent laboratory double layer experiments , 1985 .
[127] Michael J. Patterson,et al. Annular-Geometry Ion Engine: Concept, Development Status, and Preliminary Performance , 2012 .
[128] E. B. Hooper. Plasma detachment from a magnetic nozzle , 1991 .
[129] I. Boyd,et al. Modeling of anomalous electron mobility in Hall thrusters , 2006 .
[130] Vladimir Kim,et al. Dual-Mode Operation of Stationary Plasma Thrusters , 2006 .
[131] Christine Charles,et al. Measurement and modelling of a radiofrequency micro-thruster , 2012 .
[132] L. Garrigues,et al. Low frequency oscillations in a stationary plasma thruster , 1998 .
[133] M. Merino,et al. Two-dimensional supersonic plasma acceleration in a magnetic nozzle , 2010 .
[134] A. Aanesland,et al. Langmuir probe analysis of highly electronegative plasmas , 2013 .
[135] John R. Brophy,et al. Electric Propulsion for Solar System Exploration , 1998 .
[136] Michele Coletti,et al. Low Power Ablative Pulsed Plasma Thrusters , 2013 .
[137] Robert P. Hoyt,et al. Magnetic Nozzle Design for High-Power MPD Thrusters , 2005 .
[138] R. Branam,et al. Performance Evaluation of an Iodine-Vapor Hall Thruster , 2012 .
[139] Hitoshi Kuninaka,et al. Experimental Verification of the Nozzle Shape Optimization for Self-Field MPD Thruster , 2005 .
[140] M. Merino,et al. On plasma detachment in propulsive magnetic nozzles , 2011 .
[141] D. Feili,et al. Forty Years of Giessen EP-Activities and the Recent RIT-Microthruster Development , 2005 .
[142] Jason Cassibry. Comparison of Directly and Inductively Coupled Pulsed Electromagnetic Thrusters , 2008 .
[143] Christine Charles,et al. Plasmas for spacecraft propulsion , 2009 .
[144] L. Garrigues,et al. Modeling of an advanced concept of a double stage Hall effect thruster , 2008 .
[145] S. Satori,et al. Development and Demonstration of a Cathodeless Electron Cyclotron Resonance Ion Thruster , 1998 .
[146] Henry Oman,et al. Fundamentals of Electric Propulsion , 2006 .
[147] Dean Richard Massey,et al. Development of a direct evaporation bismuth Hall thruster , 2008 .
[148] I. Mikellides,et al. Conducting Wall Hall Thrusters , 2013, IEEE Transactions on Plasma Science.
[149] C. Volkmar,et al. Implementation and verification of a hybrid performance and impedance model of gridded radio-frequency ion thrusters , 2015 .
[150] R. Wirz,et al. Analytical Ion Thruster Discharge Performance Model , 2006 .
[151] I. Mikellides,et al. Magnetic Shielding of the Channel Walls in a Hall Plasma Accelerator , 2011 .
[152] L. Garrigues,et al. Electric propulsion: comparisons between different concepts , 2011 .
[153] K. Makowski,et al. Transit-time instability in Hall thrusters , 2005 .
[154] Monika Auweter-Kurtz,et al. High-Power Hydrogen Arcjet Thrusters , 1998 .
[155] Hideki Nakashima,et al. Development and Thrust Performance of a Microwave Discharge Hall Thruster , 2007 .
[156] Roger M. Myers,et al. Test facilities for high power electric propulsion , 1991 .
[157] R. Schneider,et al. The HEMPT Concept - A Survey on Theoretical Considerations and Experimental Evidences , 2011 .
[158] E. Choueiri. Plasma oscillations in Hall thrusters , 2001 .
[159] Kurt A. Polzin,et al. Ablative Z-Pinch Pulsed Plasma Thruster , 2000 .
[160] J. Adam,et al. Study of stationary plasma thrusters using two-dimensional fully kinetic simulations , 2004 .
[161] S. Tsikata,et al. Dispersion relations of electron density fluctuations in a Hall thruster plasma, observed by collective light scattering , 2009 .
[162] Maxwell G. Ballenger,et al. VASIMR ® VX-200 Performance Measurements and Helicon Throttle Tables Using Argon and Krypton , 2011 .
[163] K. H. Groh,et al. State of the art of radio‐frequency ion sources for space propulsiona) , 1994 .
[164] Lyon B. King,et al. Energetics of Propellant Options for High-Power Hall Thrusters , 2005 .
[165] Roderick Boswell,et al. Helicons-the past decade , 1997 .
[166] A. Arefiev,et al. Ambipolar acceleration of ions in a magnetic nozzle , 2007 .
[167] E. Y. Choueiri,et al. Quasi-Steady Magnetoplasmadynamic Thruster Performance Database , 2001 .
[168] Edgar Y. Choueiri,et al. Scaling of Thrust in Self-Field Magnetoplasmadynamic Thrusters , 1998 .
[169] L. Garrigues. Computational Study of Hall-Effect Thruster with Ambient Atmospheric Gas as Propellant , 2012 .
[170] M. Martinez-Sanchez,et al. Spacecraft Electric Propulsion—An Overview , 1998 .
[172] Roger M. Myers,et al. MPD thruster technology , 1991 .
[173] Robert G. Jahn,et al. Quasi-steady plasma acceleration. , 1969 .
[174] F. Levinton,et al. Ion acceleration in plasmas emerging from a helicon-heated magnetic-mirror device , 2003 .
[175] Maher I. Boulos,et al. Thermal Plasmas: Fundamentals and Applications , 1994 .
[176] Denis Estublier,et al. The SMART-1 Electric Propulsion Subsystem around the Moon: In Flight Experience , 2005 .
[177] Alec D. Gallimore,et al. Developmental Status of a 100-kW Class Laboratory Nested channel Hall Thruster , 2011 .
[178] A. Gallimore,et al. Performance and Probe Measurements of a Radio-Frequency Plasma Thruster , 2013 .
[179] E. Ahedo,et al. Theory of a stationary current-free double layer in a collisionless plasma. , 2009, Physical review letters.
[180] William B. Stein,et al. Performance Modeling of a Coaxial Radio-Frequency Gas-Discharge Microthruster , 2008 .
[181] Alec D. Gallimore,et al. Hall Thruster Cluster Operation with a Shared Cathode , 2007 .
[182] Y. Arakawa,et al. Performance Computation of a Low-Power Hydrogen Arcjet , 1999 .
[183] L. Garrigues,et al. The PEGASES Gridded Ion-Ion Thruster Performance and Predictions , 2015, IEEE Transactions on Plasma Science.
[184] Dmytro Rafalskyi,et al. Alternate extraction and acceleration of positive and negative ions from a gridded plasma source , 2014 .
[185] N. Fisch,et al. Parametric investigations of a nonconventional Hall thruster , 2001 .
[186] Robert H. Frisbee,et al. Advanced Space Propulsion for the 21st Century , 2003 .
[187] S. Mazouffre,et al. Development and experimental characterization of a wall-less Hall thruster , 2014 .
[188] K. Makowski,et al. Wall material effects in stationary plasma thrusters. II. Near-wall and in-wall conductivity , 2003 .
[189] L. Garrigues,et al. A two-dimensional (azimuthal-axial) particle-in-cell model of a Hall thruster , 2014 .
[190] M. Dudeck,et al. Wall material effects in stationary plasma thrusters. I. Parametric studies of an SPT-100 , 2003 .