Performance testing and internal probe measurements of a high specific impulse Hall thruster
暂无分享,去创建一个
[1] Yassir Azziz,et al. Instrument development and plasma measurements on a 200-watt Hall thruster plume , 2003 .
[2] Vladimir Kim,et al. Investigation of the Accelerated Ion Energy Accommodation Under Their Impingement with Solid Surfaces , 2002 .
[3] John Michael Fife,et al. Hybrid-PIC modeling and electrostatic probe survey of Hall thrusters , 1998 .
[4] Eduardo Ahedo,et al. Parametric Investigation of the Hall Thruster Discharge , 2003 .
[5] T. Haag,et al. RHETT/EPDM Performance Characterization , 1998 .
[6] H. Furth,et al. Plasma diagnostic techniques , 1965 .
[7] Anne Pacros. Instruments design and testing for a Hall thruster plume experiment on the space shuttle , 2002 .
[8] Bruce Pote,et al. Performance of a High Specific Impulse Hall Thruster , 2001 .
[9] A. Gallimore,et al. Recent Results From Internal and Very-Near-Field Plasma Diagnostics of a High Specific Impulse Hall Thruster , 2003 .
[10] Robert S. Jankovsky,et al. High Voltage SPT Performance , 2001 .
[11] Thomas W. Haag,et al. Design of a thrust stand for high power electric propulsion devices , 1989 .
[12] A. Gallimore,et al. An investigation of internal ion number density and electron temperature profiles in a laboratory-model Hall thruster , 2000 .
[13] Yevgeny Raitses,et al. Investigations of probe induced perturbations in a Hall thruster , 2002 .
[14] I. Hutchinson. Principles of Plasma Diagnostics , 1987 .
[15] G. Appelbaum,et al. Probe measurements of plasma properties inside an experimental Hall thruster , 1998 .
[16] James Joseph Szabo,et al. Fully kinetic numerical modeling of a plasma thruster , 2001 .
[17] V. Kim,et al. Local Plasma Parameter Measurements by Nearwall Probes Inside the SPT Accelerating Channel Under Thruster Operation with Kr , 2002 .
[18] Robert S. Jankovsky,et al. NASA's Hall Thruster Program 2002 , 2002 .