FIELD: transport.
SUBSTANCE: invention relates to aerospace engineering and may be used in clustered rocket bodies as a correction engine. Proposed engine comprises tank filled with working fluid and having the bore in cover, chamber and jet nozzle. Working fluid phase splitter is arranged inside the engine chamber, at tank outlet. Control valve with spring and electromagnet is arranged downstream of said splitter. This engine incorporates the device to heat working fluid in area adjoining the tank outlet. Fluid-gas engine generates jet thrust by outflow of water steam formed at gas vaporisation from liquid phase.
EFFECT: thrust adjustment, lower power consumption, non-polluting working fluid.
2 cl, 1 dwg
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