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Estimation of the Rejection Boundaries of the Spacecraft Schematic Layout by Thermal and Erosive Effects Level of the Electric Rocket Engines Plasma Jets
Authors: Nadiradze А.B., Dudunov А.А. | Published: 27.03.2023 |
Published in issue: #1(144)/2023 | |
DOI: | |
Category: Aviation and Rocket-Space Engineering | Chapter: Thermal, Electric Jet Engines, and Power Plants of Aircrafts | |
Keywords: electric rocket engine, plasma jet, thermal effect, erosive effect, allowable effect level, rejection boundary |