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Mitchell L. R. Walker
Mitchell L. R. Walker
Georgia Institute of Technology
Bestätigte E-Mail-Adresse bei ae.gatech.edu - Startseite
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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
2862018
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
1482017
High-power, null-type, inverted pendulum thrust stand
KG Xu, MLR Walker
Review of Scientific Instruments 80 (5), 2009
1422009
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
1392017
Recommended Practice for Pressure Measurements and Calculation of Effective Pumping Speeds during Electric Propulsion Testing
JW Dankanich, M Walker, MW Swiatek, JT Yim
107*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
832005
Effects of facility backpressure on the performance and plume of a Hall thruster
MLR Walker
University of Michigan, 2005
742005
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
712013
Effect of secondary electron emission on the plasma sheath
S Langendorf, M Walker
Physics of Plasmas 22 (3), 2015
702015
Thrust measurements of a radio frequency plasma source
LT Williams, MLR Walker
Journal of Propulsion and Power 29 (3), 520-527, 2013
702013
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
65*
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
632001
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
592016
Review of Plasma-Induced Hall Thruster Erosion
NP Brown, MLR Walker
Applied Sciences 10 (11), 3775, 2020
542020
A review of research in low earth orbit propellant collection
LA Singh, MLR Walker
Progress in Aerospace Sciences 75, 15-25, 2015
502015
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
502007
Background flow model of Hall thruster neutral ingestion
JD Frieman, TM Liu, MLR Walker
Journal of Propulsion and Power 33 (5), 1087-1101, 2017
492017
Effect of anode temperature on hall thruster performance
CF Book, MLR Walker
Journal of Propulsion and Power 26 (5), 1036-1044, 2010
442010
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
442006
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
432017
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