Maximum Flight Distance Of 5000m Payload Of 10kg Hybrid Fixed Wing Unmanned Aerial Vehicle
Ⅰ. Product Overview
The HX-102 uses a gasoline-electric hybrid power train to reach six hours of endurance while carrying 10 kg of sensors. Vertical take-off and landing eliminate runway dependency for long-range corridor mapping and communication relay.
Ⅱ. Key Features
- 6 h empty / 4 h fully-loaded endurance at 180 km h⁻¹ cruise
- 42 dm³ rapid-detach fuel tank, 95 RON gasoline, flame-out automatic electric backup
- 4.2 m wingspan with flaperons, stall speed 17 m s⁻¹
- Redundant starter-generators; single-engine failure still supplies 3 kW to motors
- Payload rail accepts dual EO gimbal, SAR, or 10 kg relay dish
Ⅲ. Customer Benefits
50 km dual-band datalink; field swap of engine or battery in 15 min; open MAVLink interface.
Ⅳ. Technical Data
|
project |
parameter values |
|
Wingspan |
4 200 mm |
|
Fuselage length |
2200 mm |
|
Empty weight |
55 kg (battery inside) |
|
Max take-off weight |
65 kg |
|
Max payload |
10 kg |
|
Endurance |
> 6 h (empty), > 4 h (5 kg) |
|
Max climb rate |
5 m/s |
|
Cruise speed |
40 m/s(144km/h) |
|
Service ceiling |
5 000 m (above sea level) |
|
Control radius |
50 km (line-of-sight) |
|
Operating temp |
-20 °C to +50 °C |
|
Rain limit |
light rain |
|
Wind limit |
Level 6 |
|
Flight Modes |
Manual / Fully Autonomous |
|
Takeoff Mode |
Vertical Takeoff and Landing (VTOL) |
|
Optional Payloads |
Pod Synthetic Aperture Radar (SAR)Communication Relay |
|
Propulsion Type |
Electric |
Ⅴ. Project Presentation
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