used for the main oxidizer shut-off valve of liquid rocket engines. In order to perform
numerical analysis, a pneumatic supply system was simulated as an orifice with a diameter
of 3.2 mm and the equations of motion of valve moving part were derived. For the validation
of the study, a comparison of numerical predictions and experimental results has been done.
As one of the practical applications of this study, the employment of an orifice in a high …