Applied-field MPD thruster performance with hydrogen and argon propellants

作者: Roger M. Myers

DOI: 10.2514/3.23691

关键词: Thermal conductivitySpecific impulseNuclear engineeringArgonElectrical engineeringPropellantHydrogenField (physics)Materials science

摘要:

参考文章(5)
T. W. Haag, Thrust stand for high‐power electric propulsion devices Review of Scientific Instruments. ,vol. 62, pp. 1186- 1191 ,(1991) , 10.1063/1.1141998
James S. Sovey, Mans A. Mantenieks, Performance and lifetime assessment of magnetoplasmadynamic arc thruster technology Journal of Propulsion and Power. ,vol. 7, pp. 71- 83 ,(1991) , 10.2514/3.23296
Yoshihiro Arakawa, Akihiro Sasoh, Steady-state MPD arc thruster with a permanent magnet Journal of Propulsion and Power. ,vol. 4, pp. 287- 288 ,(1988) , 10.2514/3.23063
R. J. SOVIE, D. J. CONNOLLY, Effect of background pressure on magnetoplasmadynamic thruster operation Journal of Spacecraft and Rockets. ,vol. 7, pp. 255- 258 ,(1970) , 10.2514/3.29916
ROGER MYERS, Applied-field MPD thruster geometry effects 27th Joint Propulsion Conference. ,(1991) , 10.2514/6.1991-2342