Experimental Study of Working Process in Combustion Chamber of Low-thrust Engine using Gaseous Components Methane + Oxygen

Authors: Antonov Yu.V., Yagodnikov D.A., Novikov A.V., Lapitskiy V.I., Burkaltsev V.A. Published: 22.01.2014
Published in issue: #2(67)/2007  


Category: Simulation of Processes  

Results of firing bench tests of the rocket low-thrust engine using gaseous methane and oxygen are given. It was established by experiments, that high values of perfection degree of working process were reached for this fuel. The comparative analysis of results of experiments and numerical simulation of working processes in the low-thrust rocket engine chamber is performed.