FIELD: rocket technics.
SUBSTANCE: invention relates to rocket engineering. Method of throttle control of liquid propellant system drive, based on reducing mass flow of fuel components into a chamber with uncontrolled nozzles, at which, after reducing mass flows below the set values, gas is supplied to cavity of the chamber supply lines at inputs to chamber injector head and it is mixed with liquid fuel components, creating homogeneous finely divided emulsions of fuel components, relative volumetric gas contents of which increase with increasing throttle control ratio.
EFFECT: invention provides a reduction in losses of specific impulse of liquid rocket engine with deep throttle control of drive and increase in the throttle control ratio of drive.
1 cl, 1 dwg
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