Экспериментальное исследование рабочего процесса в камере ракетного двигателя малой тяги на газообразных компонентах топлива метан + кислород

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. Refs.10. Figs.4.