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Parametric Calculation of the Limiting Characteristics of Electrization of Structural Elements of the Solid Propellant Rocket Engine Exhaust Duct
Authors: Fedotova K.V., Yagodnikov D.A. | Published: 17.04.2024 |
Published in issue: #1(148)/2024 | |
DOI: | |
Category: Aviation and Rocket-Space Engineering | Chapter: Thermal, Electric Jet Engines, and Power Plants of Aircrafts | |
Keywords: weakly ionized plasma, electrization, power condensed system, floating potential, double electric layer |