AIAA 2000-3810 Ion Propulsion Development Activities at NASA Glenn Research Center

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[2]  J. Polk,et al.  NSTAR flight thruster qualification testing , 1998 .

[3]  Michael J. Patterson,et al.  Performance of 10-kW class xenon ion thrusters , 1988 .

[4]  FMT-2 discharge cathode erosion rate measurements via laser- induced fluorescence , 2000 .

[5]  P. K. Ray,et al.  Low-Energy Sputtering Research , 1999 .

[6]  Luis R. Pinero,et al.  Development Status of a Power Processing Unit for Low Power Ion Thrusters , 2000 .

[7]  M. Patterson,et al.  Validation of the NSTAR Ion Propulsion System on the Deep Space One Mission: Overview and Initial Results , 1999 .

[8]  Michael J. Patterson,et al.  The 2.3 kW Ion Thruster Wear Test , 1995 .

[9]  Michael J. Patterson,et al.  Magnetic circuit for enhanced discharge chamber performance of a small ion thruster , 1998 .

[10]  Michael J. Patterson.  Low-Power Ion Thruster Development Status , 1998 .

[11]  Michael J. Patterson,et al.  Scaling of Ion Thrusters to Low Power , 1998 .

[12]  Michael J. Patterson,et al.  Performance of titanium optics on a NASA 30 cm ion thruster , 2000 .

[13]  Michael J. Patterson,et al.  Ion engine development for interstellar precursor missions , 2000 .

[14]  George J. Williams,et al.  CHARACTERIZATION OF THE FMT-2 DISCHARGE CATHODE PLUME , 2000 .

[15]  Michael J. Patterson,et al.  Enhanced Discharge Performance in a Ring Cusp Plasma Source , 2000 .

[16]  M. J. Mandell,et al.  Sensitivity of hollow cathode performance to design and operating parameters , 1999 .