FIELD: power industry.
SUBSTANCE: simulator of electric rocket plasma propulsion plant includes simulators of energy consumption parametres of electric gas supply valve, actuating device of gas supply control, ignited and discharge intervals of engine, storage systems of working agent, functional properties of electric gas supply valve, actuating device of gas supply control and ignited interval of engine. They are all connected along the inlet to outlet outputs of the appropriate simulators of energy consumption parametres of elements of electric rocket propulsion plant. Outlets of simulators of functional properties of actuating device of gas supply control and ignited interval of engine are connected to common control input of transistor simulator of plasma conductivity. The second output of simulator of actuating device of gas supply control is connected to output of simulator of properties of electric gas supply valve. The second input of the letter and the first input of the simulator specifying the abnormal plasma conductivity are connected to common output of simulator of storage system of working agent. The second input of simulator setting device is connected to external control device of simulator setting device. Its output is connected to common control input of transistor simulator of plasma conductivity.
EFFECT: enlarging functional capabilities of simulator.
