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Advanced Propulsion for Geostationary Orbit Insertion and North-South Station Keeping
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Options for the Human Exploration of Mars Using Solar Electric Propulsion
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Preliminary Evaluation of a 10 kW Hall Thruster
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AIAA-99-0456, Reno, NV, Jan 11- 14
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Jankovsky, R.S.1
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10
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Development and Characterization of Small SPT
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th Joint Propulsion Conference
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11
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84963799156
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SPT-115 Development and Characterization
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AIAA-99- 2568, Los Angeles, CA, June 20-24
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12
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84963852396
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Development of the BPT Family of U.S.-Designed Hall Current Thrusters for Commercial LEO and GEO Applications
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AIAA- 98-3338, Cleveland, OH, July 13-15
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14
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84962856928
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Operational Characteristics of the SPT-140 Hall Thruster
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AIAA-97-2919, Seattle, WA, July 6-9
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Manzella, D.1
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15
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85085403672
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1000 Hours of Testing on a 10 Kilowatt Hall Effect Thruster
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AIAA-2001-3773, Salt Lake City, UT, July 8-11
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th Joint Propulsion Conference
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84913571168
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Testing of a U.S.-Built HET System for Orbit Transfer Applications
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AIAA-99-2574, Los Angeles, CA, June 20-24
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th Joint Propulsion Conference
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McVey, J.B.2
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17
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72149095640
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Performance of an 8 kW Hall Thruster
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th International Electric Propulsion Conference
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Pote, B.1
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RHETT2/EPDM Development Testing
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th International Electric Propulsion Conference
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Sankovic, J.M.1
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19
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AIAA-2001-3888, Salt Lake City, UT, July 8-11
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20
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33746907697
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Characteristics of a Two-Stage Ion Accelerator with an Anode Layer
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Power Processing Unit for Stationary Plasma Thruster
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Transport-Property Measurements in the Plume of an SPT-100 Hall Thruster
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Measurement of Double Charged Ions in the Beam of a 30-cm Mercury Bombardment Thruster
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(1973)
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Vahrenkamp, R.P.1
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