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BDPT-EZY-HM-HX82 Fleetable Unmanned Helicopter

BDPT-EZY-HM-HX82 Squadable Unmanned Helicopter

BDPT-EZY-HM82 Swarm-capable unmanned helicopter featuring excellent aerodynamics, precision manufacturing, intelligent and reliable takeoff/landing systems, custom electronics, superior anti-jamming capabilities, high-reliability avionics, and exceptional stealth across radar, thermal, acoustic, visual, and radio spectrums. Easy to operate and maintain.

Product Specifications

Main Rotor Diameter:

2700MM

Total Length:

Length: 2.6 m × Width: 0.86 m × Height: 0.86 m (excluding main rotor)

Maximum width:

Standard landing gear: 860mm; High landing gear: 900mm

Maximum Height:

Standard landing gear: 860mm; High landing gear: 1160mm

 

Powertrain

Engine Type

Liquid-cooled piston

cylinder

Twin-cylinder flat

Fuel Type

Automotive gasoline 92-95#

Displacement

210cc

Cooling Method

Liquid Cooling (Forced Circulation Pump)

Start-up Method

Airborne electric start (manual; remote optional)

 

 

Power Supply System

 

Aircraft Power Supply Type

Lithium Iron Phosphate (Li-Fe) Battery 7000mAh

Voltage

12V

Airborne Generator Power

12V 300W

 

Aircraft Weight and Payload

 

Body Weight

46kg (excluding fuel)

Maximum Takeoff Weight

82KG

Typical Payload

20 KG

 

Flight Characteristics

Cruise Speed

100Km/h

Maximum Rate of Climb

3 m/s

Maximum level flight speed

120Km/h

Maximum Takeoff Altitude

Elevation 2500m

Typical battery life

120 minutes @ 20kg load (sea level)

Service ceiling

3000M

Takeoff and Landing Method

Remote takeoff and landing, smart autonomous takeoff and landing, fully autonomous takeoff and landing

Maximum Wind Resistance

Maximum wind resistance in autonomous position hold: 7 level (wind speed 16 m/s)

Formation Flight Capability

Yes

 

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Pricing Details

Product price is negotiable and determined by order quantity, configuration requirements, and delivery terms.

Submit an inquiry using the form below. Our expert team will provide a detailed quote within 24 hours.

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Product Details

 

Powertrain

 

 

Power Supply System

 

 

Aircraft Weight and Payload

 

 

Flight Characteristics

 

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