Modeling the working process in the chamber and calculating the characteristics of a low-thrust rocket engine working on the oxygen-methane gaseous propellant components with the 50 N thrust
Published: 23.06.2025
Authors: Vorozheeva O.A., Koptev I.I., Yagodnikov D.A.
Published in issue: #6(162)/2025
Category: Aviation and Rocket-Space Engineering | Chapter: Thermal, Electric Jet Engines, and Power Plants of Aircrafts