Unmanned Helicopter - Shark I

The appearance and structure of the flying shark unmanned helicopter of Hanhe Aviation have adopted a number of patented technol - details see: https://www.vehicleto.com/unmanned-helicopter-10000007
Type: HelicopterCondition: NewYear Built: 2010Place of Origin: Jiangsu China (Mainland)
Model Number: Shark I   
Unmanned Helicopter
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Dry Weight(without shell)[Kg]16.35Including Main Rotor
Cross Weight[Kg]35Including Standard Fuel

and Flight Control Unit

Task Payload Capacity[Kg]12
Weight of RC Receiver Equipment[Kg]0.6Including Battery(2h)
Weight of SAPU equipment Unit[Kg]0.85Including Battery(2h)
Two Standard Fuel Tanks[L]5[2.5x2]Extensible, anti-static
Main Rotor Diameter[mm]2146Material: Carbon Fiber
Tail Rotor Diameter[mm]403Material: Carbon Fiber
Fuel Consumption[cc/h]4000Mean(90%Load)
Gear Ratio6.88/1/4.69Engine/Main Rotor/Tail Rotor
Start-up ModeMotor and BatteryExternal Dedicated Starter
Gasoline Engine[cc]80Air-cooled, twin cylinder
Fuel[Octane]97Gasoline Fuel without Lead
Total Length[mm]2630
Total Height[mm]711
Total Width[mm]540
Servo Numbers-5
Battery Duration[h]2.0Continuous work

(without generators)

Ignition Mode--Electromagnetic Mode
Payload Mount--Aluminum Alloy

/Shock Absorber

Tail’s Material and Structure--Aluminum Alloy

/ShaftTransmission Mode

Transport Box Size


[m]3*0.56*0.78Overall Size of

Transport Box

Stability-Increasing Camera Mount

3 axis remote control

Can install video transmitter

Performance(Manual Operation)

Maximum Cruising Speed[Km/h]90
Average Cruising Speed[Km/h]65
Maximum Flying Height[m]2500
Rate of Climb[m/s]4Payload>4kg

Load Efficiency Estimate

(According to Elevation)

[%]1000m(Mean Sea Level)
Temperature Range[°C]-20+50Standard Version
Maintenance Intervals[h]100Actual Flight Time
Servo Maintenance Intervals--Reference to Manufacturer Data
Testing Time Before Delivery[h]4

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