Maximum power takeoff(S/L static;ISA) Thrust, kgf ..........................……….
The power distribution unit has a critical task to ensure that the 220VAC, 50 Hz
UAV Drone Gasoline Engine The Drone Gasoline Engine is an internal combustion en
Intellectual Property (IP) Core is a logic or data block used to build a Field P
Takeoff (S/L static;ISA), uninstalled Thru. k..............7,500...........7,500
Cockpit Dimmer Unit provides control of the integral lighting of Overhead, Instr
Flight Control System is capable of controlling flight control software, periphe
Takeoff(S/L static;ISA) Output shaft power, ehp......................….........5
The unit is used to control the camera module in the UAV. It helps the pilot in
Linear Servo Actuator Control System is used to precisely control the linear typ
Takeoff (S/L static;ISA) Output shaft power, e....................2,550.........
(S/Lstatic;ISA) Aircraft electric system DC power, kW ..........3 Bleed airflow,
(S/L static;ISA) Bleed airflow, kg/s .............................…..…..….......
Specific fuel consumption by 15...20% lower than that of current engines in this
Takeoff(S/L static;ISA) Output shaft power, ehp .......................2,500 Equ
Takeoff (S/L static;ISA) Output shaft power, ehp ........ 4,000 ............4,25
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