| Year |
Citation |
Score |
| 2017 |
Jackson BA, Terhune KJ, King LB. Ionic liquid ferrofluid interface deformation and spray onset under electric and magnetic stresses Physics of Fluids. 29: 064105. DOI: 10.1063/1.4985141 |
0.307 |
|
| 2016 |
Terhune KJ, King LB, He K, Cumings J. Radiation-induced solidification of ionic liquid under extreme electric field. Nanotechnology. 27: 375701. PMID 27487731 DOI: 10.1088/0957-4484/27/37/375701 |
0.402 |
|
| 2014 |
King LB, Meyer E, Hopkins MA, Hawkett BS, Jain N. Self-assembling array of magnetoelectrostatic jets from the surface of a superparamagnetic ionic liquid. Langmuir : the Acs Journal of Surfaces and Colloids. 30: 14143-50. PMID 25372842 DOI: 10.1021/La503341P |
0.695 |
|
| 2014 |
Hopkins MA, King LB. Magnesium hall thruster with active thermal mass flow control Journal of Propulsion and Power. 30: 637-644. DOI: 10.2514/1.B34888 |
0.338 |
|
| 2014 |
Hopkins MA, King LB. Assessment of plasma impedance probe for measuring electron density and collision frequency in a plasma with spatial and temporal gradients Physics of Plasmas. 21. DOI: 10.1063/1.4874321 |
0.301 |
|
| 2013 |
Washeleski RL, Meyer EJ, King LB. Application of maximum likelihood methods to laser Thomson scattering measurements of low density plasmas. The Review of Scientific Instruments. 84: 105101. PMID 24182157 DOI: 10.1063/1.4821980 |
0.756 |
|
| 2013 |
Meyer EJ, King LB. Electrospray from an ionic liquid ferrofluid utilizing the Rosensweig instability 49th Aiaa/Asme/Sae/Asee Joint Propulsion Conference. |
0.618 |
|
| 2012 |
Washeleski RL, Meyer EJ, King LB. Laser Thomson Scattering measurements of electron temperature and density in the near-field plume of a Hall-effect thruster 48th Aiaa/Asme/Sae/Asee Joint Propulsion Conference and Exhibit 2012. |
0.769 |
|
| 2011 |
Makela JM, Washeleski RL, King LB. Regenerable field emission cathodes: Surface morphology and performance Journal of Propulsion and Power. 27: 1097-1107. DOI: 10.2514/1.B34148 |
0.78 |
|
| 2011 |
Sommerville JD, King LB. Hall-effect thruster-cathode coupling, Part II: Ion beam and near-field plume Journal of Propulsion and Power. 27: 754-767. DOI: 10.2514/1.50124 |
0.792 |
|
| 2011 |
Sommerville JD, King LB. Hall-effect thruster-cathode coupling, Part I: Efficiency improvements from an extended outer pole Journal of Propulsion and Power. 27: 744-753. DOI: 10.2514/1.50123 |
0.771 |
|
| 2010 |
Ross JL, Sommerville JD, King LB. Energy-Loss mechanisms of a low-discharge-voltage hall thruster Journal of Propulsion and Power. 26: 1312-1317. DOI: 10.2514/1.47777 |
0.783 |
|
| 2010 |
Makela JM, Washeleski RL, Massey DR, King LB, Hopkins MA. Development of a magnesium and zinc hall-effect thruster Journal of Propulsion and Power. 26: 1029-1035. DOI: 10.2514/1.47410 |
0.742 |
|
| 2010 |
Makela JM, Washeleski RL, King LB. Re-generable field emission cathodes part II: Quenched emitter performance analyses 46th Aiaa/Asme/Sae/Asee Joint Propulsion Conference and Exhibit. |
0.767 |
|
| 2009 |
Sommerville JD, King LB. Hall-effect thruster - Cathode coupling part I: Efficiency improvements from an extended outer pole 45th Aiaa/Asme/Sae/Asee Joint Propulsion Conference and Exhibit. DOI: 10.2514/1.50123 |
0.769 |
|
| 2009 |
Makela JM, L. Washeleski R, King LB. Regenerable field emission cathode for spacecraft neutralization Journal of Propulsion and Power. 25: 970-975. DOI: 10.2514/1.41541 |
0.786 |
|
| 2009 |
Makela JM, Washeleski RL, King LB. Surface morphology and lifetime assessment of a re-generable field-emission cathode for low power electric propulsion 45th Aiaa/Asme/Sae/Asee Joint Propulsion Conference and Exhibit. |
0.769 |
|
| 2009 |
Washeleski RL, King LB. Characterization of the plasma plume from a LaB6 cathode: A comparison of probe techniques 45th Aiaa/Asme/Sae/Asee Joint Propulsion Conference and Exhibit. |
0.761 |
|
| 2009 |
Sommerville JD, King LB. Hall-effect thruster - Cathode coupling part II: Ion beam and near-field plume 45th Aiaa/Asme/Sae/Asee Joint Propulsion Conference and Exhibit. |
0.794 |
|
| 2009 |
Fossum EC, King LB. An unexamined collision-less mechanism for electron mobility in Hall thrusters 45th Aiaa/Asme/Sae/Asee Joint Propulsion Conference and Exhibit. |
0.771 |
|
| 2008 |
Sommerville JD, King LB, Chiu YH, Dressler RA. Ion-collision emission excitation cross sections for xenon electric thruster plasmas Journal of Propulsion and Power. 24: 880-888. DOI: 10.2514/1.33657 |
0.784 |
|
| 2008 |
Makela JM, Massey DR, King LB. Bismuth hollow cathode for hall thrusters Journal of Propulsion and Power. 24: 142-146. DOI: 10.2514/1.29389 |
0.767 |
|
| 2008 |
Fossum EC, King LB. An electron trap for studying cross-field mobility in Hall thrusters Ieee Transactions On Plasma Science. 36: 2088-2094. DOI: 10.1109/Tps.2008.2004231 |
0.799 |
|
| 2008 |
Fossum EC, King LB. Effects of neutral density on electron temperature and mobility in a crossed-field trap 44th Aiaa/Asme/Sae/Asee Joint Propulsion Conference and Exhibit. |
0.79 |
|
| 2008 |
Sommerville JD, King LB. Effect of cathode position on Hall-effect thruster performance and near-field plume properties 44th Aiaa/Asme/Sae/Asee Joint Propulsion Conference and Exhibit. |
0.792 |
|
| 2008 |
Makela JM, King LB. Operating characteristics of a re-generable field emission cathode for low-power Electric Propulsion 44th Aiaa/Asme/Sae/Asee Joint Propulsion Conference and Exhibit. |
0.771 |
|
| 2008 |
Massey DR, King LB, Makela JM. Development of a direct evaporation bismuth hall thruster 44th Aiaa/Asme/Sae/Asee Joint Propulsion Conference and Exhibit. |
0.745 |
|
| 2008 |
Ross JL, Sommerville JD, King LB. Efficiency analysis of a low discharge voltage Hall thruster 44th Aiaa/Asme/Sae/Asee Joint Propulsion Conference and Exhibit. |
0.772 |
|
| 2007 |
Kieckhafer A, Massey D, King LB. Performance and active thermal control of 2-kW hall thruster with segmented electrodes Journal of Propulsion and Power. 23: 821-827. DOI: 10.2514/1.21820 |
0.789 |
|
| 2007 |
Kieckhafer A, King LB. Energetics of propellant options for high-power hall thrusters Journal of Propulsion and Power. 23: 21-26. DOI: 10.2514/1.16376 |
0.305 |
|
| 2007 |
Fossum EC, King LB. Design and construction of an electron trap for studying cross-field mobility in hall thrusters Collection of Technical Papers - 43rd Aiaa/Asme/Sae/Asee Joint Propulsion Conference. 2: 1991-2005. |
0.784 |
|
| 2007 |
Sommerville JD, King LB. Effect of cathode position on hall-effect thruster performance and cathode coupling voltage Collection of Technical Papers - 43rd Aiaa/Asme/Sae/Asee Joint Propulsion Conference. 2: 1704-1714. |
0.783 |
|
| 2007 |
Makela JM, King LB. Re-generable field emission cathodes for low-power electric propulsion Collection of Technical Papers - 43rd Aiaa/Asme/Sae/Asee Joint Propulsion Conference. 2: 1680-1686. |
0.768 |
|
| 2007 |
Ross JL, King LB. Energy efficiency in low voltage hall thrusters Collection of Technical Papers - 43rd Aiaa/Asme/Sae/Asee Joint Propulsion Conference. 2: 1715-1723. |
0.448 |
|
| 2006 |
Sommerville JD, King LB. An optical diagnostic for xenon Hall thrusters including metastable contributions Collection of Technical Papers - Aiaa/Asme/Sae/Asee 42nd Joint Propulsion Conference. 7: 5035-5043. |
0.745 |
|
| 2006 |
Makela JM, Massey DR, King LB. Performance characteristics of a LaB6 bismuth cathode for use with Hall thrusters Collection of Technical Papers - Aiaa/Asme/Sae/Asee 42nd Joint Propulsion Conference. 4: 3193-3199. |
0.759 |
|
| 2006 |
Ross JL, Kieckhafer A, King LB. Performance characteristics of a low Isp Hall thruster Collection of Technical Papers - Aiaa/Asme/Sae/Asee 42nd Joint Propulsion Conference. 2: 1620-1626. |
0.468 |
|
| 2006 |
Fossum EC, King LB, Makela J. Mobility studies of a pure electron plasma in hall thruster fields Collection of Technical Papers - Aiaa/Asme/Sae/Asee 42nd Joint Propulsion Conference. 10: 8129-8143. |
0.795 |
|
| 2006 |
Kieckhafer AW, Ross JL, Massey DR, King LB. Performance characterization and ion energy analysis of a 2-kW hall thruster with segmented anodes Collection of Technical Papers - Aiaa/Asme/Sae/Asee 42nd Joint Propulsion Conference. 8: 6460-6471. |
0.772 |
|
| 2005 |
Yap YK, Kayastha V, Menda J, Vanga LK, Wang J, Kieckhafer A, Massey D, King LB. Vertically aligned carbon nanotubes as the sputter resist in space propulsive systems Materials Research Society Symposium Proceedings. 851: 53-58. DOI: 10.1557/Proc-851-Nn2.2 |
0.768 |
|
| 2004 |
King LB, Gallimore AD. Ion-Energy Diagnostics in an SPT-100 Plume from Thrust Axis to Backflow Journal of Propulsion and Power. 20: 228-242. DOI: 10.2514/1.1427 |
0.354 |
|
| 2003 |
Bollinger JJ, Kriesel JM, Mitchell TB, King LB, Jensen MJ, Itano WM, Dubin DHE. Laser-cooled ion plasmas in Penning traps Journal of Physics B: Atomic, Molecular and Optical Physics. 36: 499-510. DOI: 10.1088/0953-4075/36/3/308 |
0.355 |
|
| 2003 |
Mitchell TB, Bollinger JJ, Kriesel JM, King LB, Jensen MJ, Itano WM, Dubin DHE. Strongly correlated ion plasmas in Penning traps Journal of Physics a: Mathematical and General. 36: 6117-6118. DOI: 10.1088/0305-4470/36/22/338 |
0.395 |
|
| 2000 |
King LB, Gallimore AD. Mass spectral measurements in the plume of an SPT-100 Hall thruster Journal of Propulsion and Power. 16: 1086-1092. DOI: 10.2514/2.5681 |
0.323 |
|
| 2000 |
King LB, Gallimore AD. Ion-energy diagnostics in the plasma exhaust plume of a Hall thruster Journal of Propulsion and Power. 16: 916-922. DOI: 10.2514/2.5660 |
0.338 |
|
| 1999 |
King LB, Gallimore AD. Identifying charge-exchange collision products within the ion-energy distribution of electrostatically accelerated olasmas Physics of Plasmas. 6: 2936-2942. DOI: 10.1063/1.873251 |
0.38 |
|
| 1998 |
King LB, Gallimore AD, Marrese CM. Transport-property measurements in the plume of an SPT-100 hall thruster Journal of Propulsion and Power. 14: 327-335. DOI: 10.2514/2.5301 |
0.301 |
|
| 1996 |
Gallimore AD, Kim SW, Foster JE, King LB, Gulczinski FS. Near- and far-field plume studies of a one-kilowatt arcjet Journal of Propulsion and Power. 12: 105-111. DOI: 10.2514/3.23997 |
0.337 |
|
| 1996 |
King LB, Gallimore AD. A gridded retarding pressure sensor for ion and neutral particle analysis in flowing plasmas 32nd Joint Propulsion Conference and Exhibit. DOI: 10.1063/1.1147881 |
0.33 |
|
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