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Bruce Pote

Observed names: B. Pote, Pote, Bruce, Pote, Bruce M.
Observed institution: Busek (United States)
OpenAlex ID: A5004517591
Performance Evaluation of an Iodine-Vapor Hall Thruster
2012 · James Szabo, Bruce Pote, et al. · Journal of Propulsion and Power · 126
Development of low power Hall thrusters
1999 · V. Hruby, J. Monheiser, et al. · AIAA Plasmadynamics and Lasers Conference · 52
Iodine Plasma Propulsion Test Results at 1–10 kW
2014 · James Szabo, Mike Robin, et al. · IEEE Transactions on Plasma Science · 45
High Density Hall Thruster Propellant Investigations
2012 · James Szabo, Michael Robin, et al. · AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit (JPC) · 40
Development of the BPT family of U.S.-designed Hall current thrusters for commercial LEO and GEO applications
1998 · D. King, D. Tilley, et al. · AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit · 37
Mission and System Advantages of Iodine Hall Thrusters
2014 · John Dankanich, James J. Szabo, et al. · AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit · 30
Solar Electric Propulsion Gravity-Assist Tours For Jupiter Missions
2012 · Nathan Strange, Damon Landau, et al. · AIAA/AAS Astrodynamics Specialist Conference and Exhibit · 25
A Commercial One Newton Hall Effect Thruster for High Power In-Space Missions
2011 · James Szabo, Bruce Pote, et al. · AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit (JPC) · 24
Performance of an 8 kW Hall Thruster
2000 · B. Pote, V. Hruby, et al. · Defense Technical Information Center (DTIC) · 17
Performance Evaluation of an Iodine Vapor Hall Thruster
2011 · James Szabo, Bruce Pote, et al. · AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit (JPC) · 14
Examination of a Hall Thruster Start Transient
2002 · William Hargus, Bruce Pote · AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit (JPC) · 13
High Throughput 600 Watt Hall Effect Thruster for Space Exploration
2016 · James J. Szabo, Bruce Pote, et al. · AIAA/SAE/ASEE Joint Propulsion Conference (JPC) · 12
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Propulsion System Development for the Iodine Satellite (iSAT) Demonstration Mission
2015 · Kurt A. Polzin, Stephen R. Peeples, et al. · 12
Effect of Anode Current Fluctuations on Ion Energy Distributions within a 600 W Hall Effect Thruster
2008 · William Hargus, Michael Nakles, et al. · AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit (JPC) · 11
Performance of a multi-kilowatt non-circular discharge Hall thruster
2000 · B. Pote, V. Hruby, et al. · AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit · 10
Hall Thrusters Operating in Pulsed Mode
2001 · Vlad Hruby, Bruce Pote, et al. · 8
Eight Kilowatt Hall Thruster System Characterization
2013 · James Szabo, Bruce Pote, et al. · 7
DC-DC Converter for Hall Thruster Plasma Discharge
1999 · Vlad Hruby, Jeffery Monheiser, et al. · SAE technical papers on CD-ROM/SAE technical paper series · 7
Electromagnetic Emissions from a BHT-200 Hall Thruster
2001 · Edward J. Beiting, James E. Pollard, et al. · 4
Electromagnetic Emissions from an Engineering Model BHT-200 Thruster
2001 · E. J. Beiting, J. E. Pollard, et al. · Defense Technical Information Center (DTIC) · 2
Low-Mass, Low-Power Hall Thruster System
2015 · Bruce Pote · NASA Technical Reports Server (NASA) · 1
A Direct Drive Experiment as Part of a SEP Demonstration
2014 · William D. Deininger, Scott Enger, et al. · AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit · 1
Electrical isolation for high voltage water cooled components
1995 · Jayson G. Cordero, Vlad Hruby, et al. · OSTI OAI (U.S. Department of Energy Office of Scientific and Technical Information)
Works count: 27
Citation count: 498
H-index: 12
I10-index: 15
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