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COMMERCIAL AIRCRAFT

JH-136 Long Range VTOL Fixed Wing Drone

By Dongguan Jinhong Aviation Technology Co., Ltd. ↗

The Dongguan Jinhong Aviation Technology Co., Ltd. JH-136 is a gasoline-powered, long-range VTOL fixed-wing UAV with a 50 kg tactical load and 150 kg takeoff weight. Its configuration includes carbon fiber propellers, differential dual GPS, ESC telemetry and redundant airspeed measurement, with a maximum range of 1500 km.

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JH-136 fixed-wing drone with white wings and orange accents on a launch stand
JH-136 fixed-wing drone with white wings and orange accents on a launch stand
Takeoff weight150 kg
Wingspan2.5 m
ManufacturerDongguan Jinhong Aviation Technology Co., Ltd.
Model and platform typeJH-136 Long Range VTOL Fixed Wing Drone
Tactical load50 kg
Power system400CC two-cylinder piston EFI gasoline engine

Product overview

Dongguan Jinhong Aviation Technology Co., Ltd.’s JH-136 Long Range VTOL Fixed Wing Drone is a flight platform for long-range UAV operations. It combines vertical takeoff and landing capability with a fixed-wing architecture and carbon fiber propellers. The aircraft measures 3.5 meters in length and has a wingspan of 2.5 m. Its power system is a 400CC two-cylinder piston gasoline engine with electronic fuel injection. Tactical load is 50 kg, and takeoff weight is 150 kg.

The JH-136 incorporates a dual GPS differential design, ESC telemetry and a redundant airspeed measurement system. Navigation options include BeiDou or GPS. Its maximum range is 1500 km, with a flight altitude of 4500 meters. Cruising speed is 160 km/h, while maximum penetration speed is 180 km/h. Together, these specifications describe the aircraft’s navigation equipment, flight measurement features and principal flight figures alongside its gasoline power system, VTOL configuration and fixed-wing layout.

Specifications

SpecificationValue & conditions
ManufacturerDongguan Jinhong Aviation Technology Co., Ltd.
Model and platform typeJH-136 Long Range VTOL Fixed Wing Drone
Tactical load50 kg
Power system400CC two-cylinder piston EFI gasoline engine
Navigation systemBeiDou or GPS, etc.
Maximum range1500 km
Flight altitude4500 meters
Cruising speed160 km/h
Maximum penetration speed180 km/h
Takeoff weight150 kg
Length3.5 meters
Wingspan2.5 m
PropellersVTOL/fixed-wing carbon fiber propellers
Aerodynamic designAdvanced aerodynamic design
GPS architectureDual GPS differential design
ESC telemetryESC telemetry
Airspeed measurementRedundant airspeed measurement system
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