The BH-90 is an unmanned aerial vehicle (UAV) developed by Aero-Starloop in China.

Maximum payload is 35 kg (77 lbs).  With 60 liters of fuel capacity, the UAV is powered by a 15kw (20 hp) turbine shaft in a heavy fuel engine (HFE) propulsion system.  The aircraft is also equipped with ground collision avoidance, using a Variable Precision Rough Set (VPRS) system.  Components are modular, allowing for various configuration and upgrades.

In addition, Aero-Starloop developed a larger version: the BH-160.

Overview

Data on design, manufacture and status

Parent type: No type defined

Aircraft status: Operational

Configuration

Primary flight and mechanical characteristics

VTOL type: Helicopter

Lift devices: 1 Single main rotor

Dedicated control device: 1 Tail rotor

Crew required: 0 in Not applicable arrangement

Landing gear: Skids

Key Characteristics

Data on key physical features

Aircraft Details

Data on aircraft configuration, weights, flight performance and equipment

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Related Public Resources

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