FIELD: engines and pumps.
SUBSTANCE: invention relates to automatic fuel management systems (FMS) in fuel supply devices for liquid propellant rocket propulsion systems (RPS) of launch vehicles (LV). The proposed expenditure management system, including ROCKET fuel component installed in the feed line fuel component team choke connected links of the chain with the kinematic roller, angular position sensor link kinematic chains, reversible electric motor, rotor which is cinematically connected with the transfer roller motor and electrical signals from the sensor angular position sensor angular position link circuit control is docked on the kinematic roll throttle.
EFFECT: improvement of accuracy of work inside the motor subsystem SURT, lowering the cost of hydraulic characteristics calibration of the throttle knob of the GSS, RKS regulator, optimisation of finite values of the parameters PH-longitudinal speed and guarantee of fuel residues.
3 cl, 1 dwg
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Authors
Dates
2017-06-19—Published
2016-07-05—Filed