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Numerical Investigation of Work Cycle Characteristics in the Combustion Chamber of a Lox/Methane Liquid-Propellant Rocket Engine Featuring Reductant Power Gas Combustion
| Authors: Sidlerov D.A., Fedorov S.A. | Published: 29.06.2022 |
| Published in issue: #2(141)/2022 | |
| DOI: | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Thermal, Electric Jet Engines, and Power Plants of Aircrafts | |
| Keywords: liquid rocket engine, numerical simulation of combustion, lox/methane fuel | |