Practical and efficient
It features long endurance, high speed, long range, and a large payload capacity.
Compound-wing UAV
FCQ-150
The FCQ-150 medium-sized gasoline-powered multi-wing vertical take-off and landing unmanned aerial vehicle adopts a composite wing overall layout combining fixed wings and four-rotor wings. It solves the problem of vertical take-off and landing of fixed-wing unmanned aerial vehicles in a simple and reliable way, and combines the characteristics of long flight time, high speed, and long distance of fixed-wing unmanned aerial vehicles with the vertical take-off function of rotor-wing unmanned aerial vehicles. The vertical take-off and landing mode greatly enhances the environmental adaptability of this unmanned aerial vehicle platform. This unmanned aerial vehicle platform can operate smoothly in complex terrains such as mountains, hills, and jungles, and in areas with dense buildings, greatly expanding the application scope of unmanned aerial vehicles.
Technical Features
TECHNICAL FEATURES
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![Practical and efficient]()
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![Vertical takeoff and landing]()
Vertical takeoff and landing
It employs vertical takeoff and landing, eliminating the need for runways and requiring only a compact site for operations; moreover, its stationary hover capability significantly reduces the required operational airspace, thereby minimizing reliance on the surrounding environment.
Low operating costs
Reusable,
No complex and bulky launch and recovery equipment is required.
Easy to operate
It integrates a dedicated flight control and navigation system, enabling fully autonomous flight throughout the entire mission; it supports takeoff and landing from moving platforms and features one‑key return-to-home functionality.
Compact system
Compact layout and modular disassembly enable operation without complex auxiliary equipment, making transportation, deployment, maintenance, and dismantling straightforward.
Performance Parameters
PERFORMANCE PARAMETERS
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Wingspan
≯6300mm
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Length
≯3300mm
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Height
1200 mm (including landing gear, excluding antenna)
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Empty weight
≯100 kg (entire aircraft including engine, battery, avionics, and cabling)
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Maximum load capacity
40 kg (at sea level)
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Maximum takeoff weight
150 kg (at sea level)
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Endurance/Range
Electro-optical reconnaissance mission configuration: 10 hours; Material transport mission configuration: payload capacity of 35 kg for 4 hours.
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Cruise speed
At 150 kg, the cruise speed is 130 km/h (at an altitude of 500 meters).
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Maximum level flight speed
≮180 km/h at 2,000 m (altitude)
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Practical vertical takeoff altitude
≮2500m (takeoff weight 150kg)
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Practical ceiling
<5000m
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Takeoff and landing positioning accuracy
RTK dual-antenna, accuracy > 0.1 meter, with ground base station
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Rainproof capability
Light rain
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Operating ambient temperature
-20℃ to 55℃
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Vertical lift power motor
Brushless motor, 24S power supply
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Cruise gasoline engine
92-octane gasoline and above, electronic fuel injection, two-cylinder two-stroke, electric start, with generator
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Storage life
≥5 years
Load Configuration
LOAD CONFIGURATION
- Electro-optical reconnaissance configuration mission payload
- Material Transport Configuration Mission Payload
- Aviation Emergency Configuration Mission Payload
- Mineral Exploration Configuration Mission Payload
Application Scenarios
APPLICATION SCENARIOS
Human Shadow Meteorology
Investigation and exploration
Freight Airdrop
