Computational study of the system efficiency of supplying components in the model low-thrust rocket engine on oxygen-methane
Published: 18.10.2022
Authors: Kovalev K.E., Fedotova K.V., Vorozheeva O.A.
Published in issue: #10(130)/2022
DOI: 10.18698/2308-6033-2022-10-2217
Category: Aviation and Rocket-Space Engineering | Chapter: Thermal, Electric Jet Engines, and Power Plants of Aircrafts