Method of transient simulation of combustion processes in a low-thrust rocket engine operating on gaseous hydrogen and oxygen

V. M. Zubanov, L. S. Shabliy, D. V. Stepanov
2017 VESTNIK of the Samara State Aerospace University  
doi:10.18287/2541-7533-2016-15-4-64-74 fatcat:5gbgf6jjqjbfhfkg5nkyfubyuy