NASA NTRS · 20060038568
Experimental Evaluation of Russian Anode Layer Thrusters
Abstract
Performance and endurance testing of a 1.35 kW thruster with anode layer (TAL), developed at the Central Research Institute of Machine Building (TsNIMASH) is described.
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Garner, C. E., Polk, J. E., Brophy, J. R., Marrese, C., Semenkin, S., Tverdokhlebov, S.. 1994-06-01. Experimental Evaluation of Russian Anode Layer Thrusters. https://ntrs.nasa.gov/citations/20060038568
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