MPD thruster technology

MPD (MagnetoPlasmaDynamic) thrusters demonstrated between 2000 and 7000 seconds specific impulse at efficiencies approaching 40 percent, and were operated continuously at power levels over 500 kW. These demonstrated capabilities, combined with the simplicity and robustness of the thruster, make them attractive candidates for application to both unmanned and manned orbit raising, lunar, and planetary missions. To date, however, only a limited number of thruster configurations, propellants, and operating conditions were studied. The present status of MPD research is reviewed, including developments in the measured performance levels and electrode erosion rates. Theoretical studies of the thruster dynamics are also described. Significant progress was made in establishing empirical scaling laws, performance and lifetime limitations and in the development of numerical codes to simulate the flow field and electrode processes.

[1]  Leonard A. Dudzinski,et al.  Nuclear electric propulsion mission performance for fast piloted Mars missions , 1991 .

[2]  M. Martinez-Sanchez,et al.  Electrothermal and modified two stream instabilities in MPD thrusters , 1990 .

[3]  Monika Auweter-Kurtz,et al.  Cathode phenomena in plasma thrusters , 1987 .

[4]  E. Messerschmid,et al.  Plasma accelerator activities at the IRS , 1990 .

[5]  Edgar Y. Choueiri Electron-ion Streaming Instabilities of an Electromagnetically Accelerated Plasma , 1991 .

[6]  G. Kruelle Theoretical treatment of current, mass flow, and related distributions in MPD plumes , 1972 .

[7]  Ernst Messerschmid,et al.  Gradient driven instabilities in stationary MPD thruster flows , 1990 .

[8]  E. B. Hooper Plasma detachment from a magnetic nozzle , 1991 .

[9]  Edgar Y. Choueiri,et al.  MPD thruster plasma instability studies , 1987 .

[10]  Monika Auweter-Kurtz,et al.  Comparison of numerical and experimental investigations of nozzle type MPD accelerators , 1990 .

[11]  James E. Polk,et al.  Mechanisms of hot cathode erosion in plasma thrusters , 1990 .

[12]  H. Minakuchi Magnetoplasmadynamic Analysis of Plasma Acceleration , 1984 .

[13]  Alan H. Glasser,et al.  Characterization of Plasma Flow through Magnetic Nozzles , 1990 .

[14]  Kurt F. Schoenberg,et al.  Preliminary scoping studies for nozzle‐based coaxial plasma thrusters , 1991 .

[15]  Monika Auweter-Kurtz,et al.  Numerical evaluation of MPD thrusters , 1990 .

[16]  R. J. Goldstein,et al.  Film cooling effectiveness with helium and refrigerant 12 injection into a supersonic flow , 1970 .

[17]  R. J. Checkley,et al.  Radiation cooled MPD arc thruster , 1969 .

[18]  La Pointe,et al.  Numerical simulation of self-field MPD thrusters , 1991 .

[19]  T. W. Haag Thrust stand for high‐power electric propulsion devices , 1991 .

[20]  Manuel Martinez-Sanchez,et al.  Quasi-one-dimensional numerical simulation of magnetoplasmadynamic thrusters , 1992 .

[21]  Arnold J. Kelly,et al.  Electropositive surface layer MPD thruster cathodes , 1989 .

[22]  M. Martinez-Sanchez,et al.  Viscous and diffusive effects in MPD flows , 1990 .

[23]  Alec D. Gallimore,et al.  Anode power deposition in quasi-steady MPD thrusters , 1990 .

[24]  J. L. Lawless,et al.  Theory of onset in magnetoplasmadynamic thrusters , 1987 .

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

[26]  A. J. Kelly,et al.  Cathode phenomena in a low power, steady state MPD thruster , 1988 .

[27]  J. L. Lawless,et al.  Onset in magnetoplasmadynamic thrusters with finite-rate ionization , 1988 .

[28]  Itsuro Kimura,et al.  Current distribution and plasma acceleration in MPD arcjets with applied magnetic fields , 1988 .

[29]  Hassan Hassan,et al.  ANALYSIS OF MPD ARCS WITH NONEQUILIBRIUM IONIZATION. , 1968 .

[30]  J. L. Lawless,et al.  Electrode-adjacent boundary layer flow in magnetoplasmadynamic thrusters , 1988 .

[31]  Manuel Martinez-Sanchez,et al.  Structure of self-field accelerated plasma flows , 1991 .

[32]  M. Williams,et al.  Experiments using a 25-kw hollow cathode lithium vapor MPD arcjet , 1969 .

[33]  Roger M. Myers,et al.  Performance of a 100 kW class applied field MPD thruster , 1989 .

[34]  Hirokazu Tahara,et al.  Experimental and theoretical researches on arc structure in a self-field thruster , 1987 .

[35]  Hirokazu Tahara,et al.  Thruster performance and acceleration mechanisms of a quasi-steady applied-field MPD arcjet , 1990 .

[36]  J. H. Gilland,et al.  Evolutionary use of nuclear electric propulsion , 1990 .

[37]  R. G. Jahn,et al.  Design and development of a thermo-ionic electric thrustor Final report, 30 Apr. 1964 - 11 Jan. 1966 , 1966 .

[38]  James S. Sovey,et al.  Performance and lifetime assessment of magnetoplasmadynamic arc thruster technology , 1991 .

[39]  Jan Rosciszewski,et al.  Acceleration Process in the Hall Current Device , 1967 .

[40]  Yukio Shimizu,et al.  Idealized model for plasma acceleration in an MHD channel , 1983 .

[41]  J. Smith,et al.  Electrothermal instability - An explanation of the MPD arc thruster rotating spoke phenomenon. , 1969 .

[42]  J. H. Gilland,et al.  Multimegawatt electric propulsion system design considerations , 1990 .

[43]  Roger M. Myers,et al.  Applied-field MPD thruster geometry effects , 1991 .

[44]  M. Martinez-Sanchez,et al.  Two-dimensional numerical simulation of MPD flows , 1987 .

[45]  Itsuro Kimura,et al.  Analytical study on the influence of nonequilibrium ionization for current flow pattern and flow field of MPD arcjets , 1990 .

[46]  H. Hugel,et al.  Effect of Self-Magnetic Forces on the Anode Mechanism of a High Current Discharge , 1980, IEEE Transactions on Plasma Science.

[47]  Monika Auweter-Kurtz,et al.  Cathode Erosion Studies on MPD Thrusters , 1987 .

[48]  M. Martinez-Sanchez,et al.  A two dimensional model of an MPD thruster , 1991 .

[49]  Valery Godyak,et al.  Smooth plasma-sheath transition in a hydrodynamic model , 1990 .

[50]  A. J. Kelly,et al.  Energy deposition in low-power coaxial plasma thrusters , 1991 .

[51]  C. J. Michels,et al.  Low environmental pressure MPD arc tests. , 1968 .

[52]  Edgar Y. Choueiri,et al.  Current driven instabilities of an electromagnetically accelerated plasma , 1988 .

[53]  M. Martinez-Sanchez,et al.  Nonequilibrium ionization in plasma accelerators , 1990 .

[54]  Won-Taek Park,et al.  Numerical Analysis of MPD Arcs for Plasma Acceleration , 1987, IEEE Transactions on Plasma Science.