Aero-Starloop BH-160
The BH-160 is an unmanned aerial vehicle (UAV) developed by Aero-Starloop in China.
Maximum payload is 65 kg (143.3 lbs). With 100 liters of fuel capacity, the UAV is powered by a 30kw (40 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 lighter version: the BH-90.
Overview
Data on design, manufacture and statusDesign authority: Aero-Starloop High-Tec. Co., LTD
Primary manufacturer: Aero-Starloop High-Tec. Co., LTD
Parent type: No type defined
Aircraft status: Operational
Configuration
Primary flight and mechanical characteristicsVTOL type: Helicopter
Lift configuration: Single main rotor
Dedicated control device: Tail rotor
Crew required: 0
Crew seating: Not applicable
Landing gear: Skids
Overall Dimensions
Data on aircraft sizeOverall Width: 3.69 m (12.1 ft)
Engine Details
Aircraft powerplant (lift and/or propulsion)Total number of engines: 1
Weights and Performance
Data on aircraft weight and flight characteristicsMax Range: 350 km (189 nm)
Max Endurance: 3.5 hrs (3.5 hrs)
