• Electric Version 2.5hours Endurance Vtol Fixed Wing Aircraft
  • Electric Version 2.5hours Endurance Vtol Fixed Wing Aircraft
  • Electric Version 2.5hours Endurance Vtol Fixed Wing Aircraft
  • Electric Version 2.5hours Endurance Vtol Fixed Wing Aircraft
  • Electric Version 2.5hours Endurance Vtol Fixed Wing Aircraft

Electric Version 2.5hours Endurance Vtol Fixed Wing Aircraft

Certification: ISO9001, FCC, RoHS
Height: High Altitude
Operating Radius: Remote
Size: Large
Usage: Surveillance and Patrol
Structure: Fixed-Wing UAV
Customization:
Diamond Member Since 2014

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Basic Info.

Model NO.
KWT-F360-H
Maximum Measurement and Control Distance
40km (Los)
Maximum Level Flight Speed
100km/H
Maximum Endurance
2.5h
Maximum Takeoff Weightt25kg
Maximum Working Loadt3kg
Power System
High Efficiency Brushless Motor
Control Modetfully Autonomous Control
Fully Autonomous Control
Maximum Wind Tolerance
1500mm*610mm*540mm
Electric Version
Powered by Battery
Transport Package
Aluminum Case
Specification
carbon fiber
Trademark
ALLTECH
Origin
China
Production Capacity
5000/Year

Product Description

2.5Hours Electric Version Vertical Take-off and Landing(VTOL) Fixed Wing Aircraft KWT-F360-H
Electric Version 2.5hours Endurance Vtol Fixed Wing Aircraft

 


KWT-GM360-H vertical take-off and landing fixed wing, wingspan 3.6 meters, has electric version and hybrid version. This model combines the characteristics of long-endurance, high-speed and long-distance of fixed-wing UAVs and the vertical take-off and landing of rotor-wing drones. It does not require runway but only small space for take-off and landing, and can be operated smoothly on ship deck, narrow airspace, mountain, complex terrain and densely populated areas such as hills, jungles. The whole process of autonomous flight can be completed without operator intervention for cruise, flight state transition and vertical take-off and landing.

The equipment compartment is a replaceable hatch cover, and different mounting hole positions can be designed for different load requirements of the user.

The fuselage is designed as quick release structure, with reliable electrical connection, plug and play; unfolding and withdrawal time is less than 10 minutes.

The engine is rear-mounted and the load is placed forward to provide a larger field of view for the photoelectric load without obstruction.



  Feature
  • Easy to assemble and operate
  • Vertical take-off and landing, without limitation of space
  • Resistance to harsh weather conditions
  • Diesel-electric version and electric version optional
  • All carbon fiber composite material, industry standard architecture
  • Compatible with PC station, suitable for open source of autopilot system
Fuselage Parameters
Wingspan 3600mm
Fuselage length 2300mm
Body height 460mm (without tail)
Maximum measurement and control distance 40km (LOS)
Runway 5m*5m
Takeoff/landing vertical

Electric aircraft specifications
Maximum level flight speed 100km/H
(Sea level standard atmospheric pressure)
Cruising speed 70~100km/H
Lift limit 4500m
Maximum endurance 2h
Maximum  takeoff weight 25kg
Maximum working load 3kg
Takeoff and landing mode Vertical
Power system High efficiency brushless motor
Control mode Fully autonomous control
Maximum wind tolerance 8.0-10.7m/s
Packing box size 1500mm*610mm*540mm
Packing box:
Electric Version 2.5hours Endurance Vtol Fixed Wing Aircraft



 
 
Dual day and night camera payloads recommended, still other payloads for optional, according to user's real use requirements. 
Electric Version 2.5hours Endurance Vtol Fixed Wing Aircraft
Electric Version 2.5hours Endurance Vtol Fixed Wing Aircraft

Electric Version 2.5hours Endurance Vtol Fixed Wing Aircraft

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