Applied-Field Magnetoplasmadynamic Thrusters, Part 2: Analytic Expressions for Thrust and Voltage

作者: Pavlos G. Mikellides , Peter J. Turchi

DOI: 10.2514/2.5657

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摘要: THEassumptionthatthemainaccelerationme… by the applied-fi eld magnetoplasmadynamic (MPD) thruster is theconversionofazimuthalkineticenergytous… expansion through a magnetic nozzle was the basis for all previous theoretical efforts. 1، 3 These models, however, were not able to capture the general trends displayed by experiments. Further, as of today only one analytic model exists that attempts to predict thrust and voltage. This was a result of a mainly experimentalwork by Fradkin4 with a lithium propellant thruster. He …

参考文章(7)
David Wehrle, Mark Vernyi, Shawn Reese, Roger M. Myers, James Biaglow, A preliminary characterization of applied-field MPD thruster plumes ,(1991)
T. G. Cowling, Sydney Chapman, David Park, The mathematical theory of non-uniform gases ,(1939)
Masafumi Tanaka, Itsuro Kimura, Current distribution and plasma acceleration in MPD arcjets with applied magnetic fields Journal of Propulsion and Power. ,vol. 4, pp. 428- 436 ,(1988) , 10.2514/3.23084
Roger M. Myers, Applied-field MPD thruster performance with hydrogen and argon propellants Journal of Propulsion and Power. ,vol. 9, pp. 781- 784 ,(1993) , 10.2514/3.23691
G. BREDERLOW, R. T. HODGSON, Electrical conductivity in seeded noble gas plasmas in crossed electric and magnetic fields. AIAA Journal. ,vol. 6, pp. 1277- 1284 ,(1968) , 10.2514/3.4734