FIELD: rocket engines.
SUBSTANCE: main line of liquid propellant thruster includes propellant component feed pipeline and series-mounted in pipeline throttling device and delivery valve, and also behind-the-valve space. Used as throttling device is automatic flow governor and displacing member with movable hermetic divider installed in parallel with governor. Inlet space of divider communicate with pipeline before flow governor and outlet space communicates with pipeline after flow governor.
EFFECT: improved dynamic characteristics and stability of gaining operating conditions.
7 cl, 5 dwg
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