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A-HAWK Ⅱ

Overview

A-HAWK Ⅱ

Home / Products / A-HAWK Ⅱ / Overview

 “A-HAWK II” is a type of oil-powered heavy-duty vertical

take-off and landing multi-rotor UAV. A single oil-driven

aero-engine is used to drive four variable-distance ducted

propeller systems to work efficiently through the transmission

system. Advanced control systems and software ensure flight

stability and reliability. It has strong environmental adaptability

and is equipped with a variety of mission loads to achieve

transportation, integrated reconnaissance and strike, high-rise

fire fighting and other tasks; and it can meet the needs of

different users in  logistics, police, fire and other fields.

Home / Products / A-HAWK Ⅱ / Technical Parameters

A-HAWK Ⅱ

Technical Parameters

Wheelbase: 2300mm

Aircraft Height: 1600mm

Aircraft Length: 4320mm

Aircraft Width: 3728mm

Drone performance indicator

• Maximum Takeoff Weight: 450kg

• Mission Payload: 120kg

• Cruise Speed: 60km/h

• Lift Limit: 4h

• Time of Endurance: 30min

 

UAV environmental adaptability

Dimensions

Wind Resistance: 12m/s (takeoff and landing)

                            15m/s (flight)

Temperature:-40 ° C -70 ° C

Rainproof:Light rain (<10mm/24h)

Environment: Resistant to salt spray and sandstone

UAV system

The multi-rotor UAV combat system consists of an aircraft platform, mission system and ground control and support. The main system groups are

as follows:

A-HAWK Ⅱ

Video

Home / Products /  A-HAWK Ⅱ / Video