FIELD: rocket science.
SUBSTANCE: device (52) for regulating the flow of a working medium for an electric rocket engine of a thermocapillary device type contains at least one electrically conductive capillary channel, and it is made with the possibility of regulating the flow of a working medium under the action of change in a channel temperature. Walls of the specified at least one capillary channel are made of an alloy based on nickel.
EFFECT: obtaining a device for regulating the flow of a working medium for an electric rocket engine.
14 cl, 2 dwg
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Authors
Dates
2022-05-05—Published
2018-05-16—Filed