Product overview
The HC-141 is a complete fixed-wing flight platform built for long missions. Its composite fuselage has a high-performance aerodynamic shape and can be taken apart and reassembled, so crews can move and redeploy it quickly. An air-cooled, two-cylinder, horizontally-opposed, two-stroke, direct-drive aviation piston engine provides the power for climb and cruise. The engine draws from a 40L tank filled with 95-octane gasoline premixed at 1:50 with fully synthetic lube oil. The rated figures are up to 12 hours of endurance, a 50kg payload and wind resistance up to level 7. The operating conditions behind these figures are not stated.
An integrated flight control computer works with a micro combined GPS/INS navigation unit. Together they support one-click automatic takeoff and landing, circling, return, altitude hold and autonomous cruise along planned routes. The aircraft can also fly beyond visual range, and operators can change flight modes while it is airborne. Real-time data transmission is supported, and operators manage missions through Honeycomb's intelligent control software.
The aircraft has a universal payload platform that accepts several mission loads. One is a dual-lens gimbal with an infrared camera, a 30x visible-light camera and a laser rangefinder with a range of up to 5km. Another is a larger two-axis triple-lens targeting camera that pairs a 30x optical zoom camera with a 640×512 infrared camera and a laser rangefinder with a range of up to 3km. The other options are an airborne broadband communication base station and payloads customised by third parties.
Specifications
| Specification | Value & conditions |
|---|---|
| Platform type | Fixed-wing UAV with aviation piston engine |
| Airframe construction | High-performance aerodynamic shape with composite fuselage |
| Endurance | Up to 12 hWith 40L fuel tank |
| Payload capacity | 50kg |
| Wind resistance | Level 7 |
| Fuel tank capacity | 40L |
| Fuel composition | 95# gasoline with 1:50 fully synthetic lube oil |
| Engine type | Air-cooled, two-cylinder, horizontally-opposed, two-stroke, direct-drive aeroengine |
| Navigation | Integrated flight control computer with micro combined navigation system (GPS/INS) |
| Autonomous functions | One-click automatic takeoff, landing, circling, return, altitude hold, autonomous landing and route cruise |
| Data link | Real-time data transmission |
| Dual-lens camera option | 30x visible light camera, infrared camera, laser rangefinder up to 5kmOptional dual-lens camera payload |
| Triple-lens camera option | 30x optical zoom, 640×512 infrared camera, laser rangefinder up to 3kmOptional large triple-lens camera payload |
| Communication payload option | Airborne broadband base station for emergency communicationOptional communication base station payload |
| Third-party payloads | Supported via customization |
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