| Recent progress and perspectives of space electric propulsion systems based on smart nanomaterials I Levchenko, S Xu, G Teel, D Mariotti, MLR Walker, M Keidar Nature communications 9 (1), 879, 2018 | 267 | 2018 |
| High-power, null-type, inverted pendulum thrust stand KG Xu, MLR Walker Review of Scientific Instruments 80 (5), 2009 | 140 | 2009 |
| Recommended practice for use of Faraday probes in electric propulsion testing DL Brown, MLR Walker, J Szabo, W Huang, JE Foster Journal of Propulsion and Power 33 (3), 582-613, 2017 | 137 | 2017 |
| Recommended practice for thrust measurement in electric propulsion testing JE Polk, A Pancotti, T Haag, S King, M Walker, J Blakely, J Ziemer Journal of Propulsion and Power 33 (3), 539-555, 2017 | 131 | 2017 |
| Recommended Practice for Pressure Measurements and Calculation of Effective Pumping Speeds during Electric Propulsion Testing JW Dankanich, M Walker, MW Swiatek, JT Yim | 103* | 2013 |
| Effect of backpressure on ion current density measurements in hall thruster plumes MLR Walker, AL Victor, RR Hofer, AD Gallimore Journal of Propulsion and Power 21 (3), 408-415, 2005 | 79 | 2005 |
| Effects of facility backpressure on the performance and plume of a Hall thruster MLR Walker University of Michigan, 2005 | 73 | 2005 |
| Effect of secondary electron emission on the plasma sheath S Langendorf, M Walker Physics of Plasmas 22 (3), 2015 | 69 | 2015 |
| Recommended practices in thrust measurements JE Polk, A Pancotti, T Haag, S King, M Walker, J Blakely, J Ziemer CALIFORNIA INST OF TECHNOLOGY PASADENA JET PROPULSION LAB, 2013 | 68 | 2013 |
| Thrust measurements of a radio frequency plasma source LT Williams, MLR Walker Journal of Propulsion and Power 29 (3), 520-527, 2013 | 67 | 2013 |
| The effects of nude faraday probe design and vacuum facility backpressure on the measured ion current density profile of hall thruster plumes. pages AIAA 2002 4253 … MLR Walker, RR Hofer, AD Gallimore 38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, 0 | 64* | |
| A Comparison of nude and collimated Faraday Probes for Use with Hall Thrusters RR Hofer, MLR Walker, AD Gallimore 27th International Electric Propulsion Conference, 01-020, 2001 | 62 | 2001 |
| Electrical facility effects on Hall thruster cathode coupling: Performance and plume properties JD Frieman, JA Walker, MLR Walker, V Khayms, DQ King Journal of Propulsion and Power 32 (1), 251-264, 2016 | 56 | 2016 |
| Performance characteristics of a cluster of 5-kW laboratory Hall thrusters MLR Walker, AD Gallimore Journal of Propulsion and Power 23 (1), 35-43, 2007 | 50 | 2007 |
| Review of Plasma-Induced Hall Thruster Erosion NP Brown, MLR Walker Applied Sciences 10 (11), 3775, 2020 | 49 | 2020 |
| A review of research in low earth orbit propellant collection LA Singh, MLR Walker Progress in Aerospace Sciences 75, 15-25, 2015 | 47 | 2015 |
| Background flow model of Hall thruster neutral ingestion JD Frieman, TM Liu, MLR Walker Journal of Propulsion and Power 33 (5), 1087-1101, 2017 | 46 | 2017 |
| Effect of anode temperature on hall thruster performance CF Book, MLR Walker Journal of Propulsion and Power 26 (5), 1036-1044, 2010 | 43 | 2010 |
| Magnetically filtered Faraday probe for measuring the ion current density profile of a Hall thruster JL Rovey, MLR Walker, AD Gallimore, PY Peterson Review of Scientific Instruments 77 (1), 2006 | 43 | 2006 |
| Electric propulsion reliability: Statistical analysis of on-orbit anomalies and comparative analysis of electric versus chemical propulsion failure rates JH Saleh, F Geng, M Ku, MLR Walker II Acta Astronautica 139, 141-156, 2017 | 42 | 2017 |
Samuel LangendorfScientist, Los Alamos National Laboratory在 lanl.gov 的电子邮件经过验证
