Low-Power Ion Propulsion for Small Spacecraft

Michael J. PattersonLewis Research Center, Cleveland, OhioSteven R. OlesonNYMA, Inc., Brook Park, OhioPrepared for the33rd Joint Propulsion Conference and Exhibitcosponsored by AIAA, ASME, SAE, and ASEESeattle, Washington, July 6-9, 1997National Aeronautics andSpace AdministrationLewis Research Center

[1]  J. Power,et al.  Planned flight test of a mercury ion auxiliary propulsion system. 1: Objectives, systems descriptions, and mission operations , 1978 .

[2]  Michael J. Patterson,et al.  Derated ion thruster design issues , 1991 .

[3]  Michael J. Patterson,et al.  NASA 30 Cm Ion Thruster Development Status , 1994 .

[4]  D. C. Byers,et al.  Primary electric propulsion for future space missions , 1979 .

[5]  Steven J. Isakowitz,et al.  International Reference Guide to Space Launch Systems , 1991 .

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

[7]  Michael J. Patterson,et al.  Performance of the NASA 30 cm Ion Thruster , 1993 .

[8]  S. Schneider,et al.  Small Satellite Propulsion Options , 1994 .

[9]  B. Agrawal Design of Geosynchronous Spacecraft , 1986 .

[10]  Michael J. Patterson Low-Isp derated ion thruster operation , 1992 .

[11]  Roger M. Myers,et al.  A 100 Hour Wear Test of the NASA NSTAR Ion Thruster , 1996 .

[12]  Michael J. Patterson,et al.  Performance and optimization of a derated ion thruster for auxiliary propulsion , 1991 .

[13]  David Steffy ORBCOMM Satellites Launch and Initial Flight Operations , 1996 .

[14]  Roger M. Myers,et al.  Advanced Propulsion for Geostationary Orbit Insertion and North-South Station Keeping , 1997 .

[15]  John M. Sankovic,et al.  Evaluation of Low Power Hall Thruster Propulsion , 1996 .

[16]  Robert Meurer First Class Science on a Coach Class Ticket , 1995 .

[17]  James S. Sovey Improved ion containment using a ring-cusp ion thruster , 1984 .

[18]  Dennis L. Tilley,et al.  Benefits of Low-Power Stationary Plasma Thruster Propulsion for Small Satellites , 1995 .