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In a valve control unit for a ram jet propulsion system having a power unit space a valve for controlling a fuel quantity required to the propulsion system, and a valve adjusting unit which is constructed to be operable by means of an electronic control unit, the valve is combined with its valve adj

In a valve control unit for a ram jet propulsion system having a power unit space a valve for controlling a fuel quantity required to the propulsion system, and a valve adjusting unit which is constructed to be operable by means of an electronic control unit, the valve is combined with its valve adjusting unit and its electronic control unit to form a thermally insulated valve assembly. The valve assembly is configured for the arrangement in the power unit space.

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1. A valve control unit for a ram jet propulsion system of a missile comprising a power unit space, the valve control unit comprising: a valve configured to control a fuel quantity required for the propulsion;a valve adjusting unit configured to control the valve;an electronic control unit comprisin

1. A valve control unit for a ram jet propulsion system of a missile comprising a power unit space, the valve control unit comprising: a valve configured to control a fuel quantity required for the propulsion;a valve adjusting unit configured to control the valve;an electronic control unit comprising a signal processing unit configured to control the valve adjusting unit;an electromotive drive;a housing; anda constructional body having a cylindrical disk shape, whereinthe valve, the valve adjusting unit, the electromotive drive, and the electronic control unit are configured together within the housing with an air gap between the valve, valve adjusting unit, electromotive drive, and electronic control unit and the housing to form a thermally insulated valve assembly,the valve assembly is arranged in a recess of the constructional body, andthe constructional body is configured for arrangement in the power unit space, which is between a combustion chamber and fuel chamber, with a circumference of the constructional body corresponding to a circumference of an exterior of a housing of the missile. 2. The valve control unit according to claim 1, further comprising an electromotive drive having a servo motor which is connected with a threaded spindle; wherein:a spindle gearing part is provided on the threaded spindle which can be displaced in the longitudinal direction of the threaded spindle; and the threaded spindle is connected by means of a lever element with a valve shaft that defines a 90° angle with respect to an axis of the spindle drive. 3. The valve control unit according to claim 1, wherein: the electronic control unit comprises a controlling part having a desired phase value unit, a correction controller and an error detection unit for polar values;the desired phase control unit is fed at its input, on the one hand, with one of polar current commands and voltage commands, and on the other hand, with a correction signal of the correction controller;the correction controller is connected with the error detection unit; andthe error detection unit is supplied with desired and actual values. 4. The valve control unit according to claim 1, wherein the electronic control unit is provided with at least one sensor interface having a signal processing unit that includes a semiconductor bridge circuit for controlling a driving motor for controlling the fuel quantity required for the propulsion. 5. The valve control unit according to claim 3, wherein the electronic control unit has a potential separation between a semiconductor bridge and the signal processing unit. 6. The valve control unit according to claim 1, wherein: the electronic control unit has current sensors for measuring a motor current of the driving motor;the current sensors monitor or correct the motor current; andthe measured current is fed to a signal processing unit. 7. The valve control unit according to claim 1, wherein the electric control unit contains a PWM control of the driving motor.