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Methods for Assessing Parameters of the Stationary Plasma Engine Plume Multifractional Model Based on the Results of Probe Measurements
Authors: Nadiradze A.B., Frolova Yu.L. | Published: 27.03.2021 |
Published in issue: #1(136)/2021 | |
DOI: | |
Category: Aviation and Rocket-Space Engineering | Chapter: Thermal, Electric Jet Engines, and Power Plants of Aircrafts | |
Keywords: stationary plasma thruster, plume multifractional model, electrostatic probe --- energy analyzer, braking characteristic, angular characteristic, smoothing |