Regenerative Cooling Comparison of LOX/LCH<sub>4</sub> and LOX/LC<sub>3</sub>H<sub>8</sub> Rocket Engines Using the One-Dimensional Regenerative Cooling Modelling Tool ODREC

Regenerative Cooling Comparison of LOX/LCH<sub>4</sub> and LOX/LC<sub>3</sub>H<sub>8</sub> Rocket Engines Using the One-Dimensional Regenerative Cooling Modelling Tool ODREC

Due to the extreme temperatures inside the combustion chambers of liquid propellant rocket engines, the walls of the combustion chamber and the nozzle are cooled by either the fuel or the oxidizer in what is known as <i>regenerative cooling</i>. This study presents an indigenous computat...

Full description

Bibliographic Details
Main Authors: Yigithan Mehmet Kose, Murat Celik
Format: Article
Language:English
Published: MDPI AG 2023-12-01
Series:Applied Sciences
Subjects:
rocket propulsion
regenerative cooling
heat transfer modelling
LOX/LCH<sub>4</sub> rocket engines
LOX/LC<sub>3</sub>H<sub>8</sub> rocket engines
Online Access:https://www.mdpi.com/2076-3417/14/1/71

Internet

https://www.mdpi.com/2076-3417/14/1/71

Similar Items