The H200P is a medium-long-range delivery catapult-launch fixed-wing UAV.
It takes off by catapult without a runway, offering flexible deployment.
It has a wingspan of 2545 mm, a fuselage length of 3400 mm, a height of 640 mm, an empty weight of 90 kg, a maximum takeoff weight of 200 kg, a maximum payload of 135 kg (including fuel) and a fuel tank capacity of 115 L.
The fuel tail-push power system with built-in electric start delivers an endurance of up to 720 minutes and a maximum range of 2280 km.
Its service ceiling reaches 4000 m, with a maximum speed of 220 km/h and a cruise speed of 180-200 km/h.
The climb rate is <=3.5 m/s and the descent rate is <=3 m/s.
The aircraft withstands level-6 winds, offers an IP54 rating and operates from -25°C to +45°C, adapted for low-temperature operations.
The airframe is built of fiberglass composite for durability.
Dual GNSS positioning modules, dual IMUs and dual gyroscopes are built into the flight controller for high flight-safety redundancy.
It supports RTK/PPK differential systems with a customizable telemetry range of 15/30/50 km to meet high-precision mission needs.
It is well suited for applications such as ultra-long-range cargo delivery and inspection.


H200P Medium-Long-Range Delivery Catapult Launch Fixed-Wing UAV, 720 min Endurance, 2280 km Range
The H200P is a medium-long-range delivery catapult-launch fixed-wing UAV with fuel tail-push propulsion, a 200 kg MTOW, a 135 kg payload (including fuel) and a 115 L fuel tank, an endurance of up to 720 minutes and a 2280 km range; it operates in -25°C low-temperature environments, making it ideal for ultra-long-range cargo delivery.
Original price was: $68,500.00.$53,400.00Current price is: $53,400.00.
| Product Positioning | Medium/Long-Range Delivery |
|---|---|
| Takeoff/Landing Mode | Catapult Launch |
| Power System | Fuel-Powered |
| Start Mode | Built-In Electric Start |
| Cruise Power | Fuel Tail-Push Propeller |
| Wingspan (mm) | 2545 |
| Fuselage Length (mm) | 3400 |
| Height (mm) | 640 |
| MTOW (kg) | 200 |
| Empty Weight (kg) | 90 |
| Max Payload (kg) | 135 (incl. fuel) |
| Fuel Tank Capacity (L) | 115 |
| Endurance | 720 min |
| Max Range (km) | 2280 |
| Service Ceiling (m) | 4000 |
| Max Speed (km/h) | 220 |
| Cruise Speed (km/h) | 180-200 |
| Climb Rate (m/s) | <=3.5 |
| Descent Rate (m/s) | <=3 |
| Wind Resistance | Level 6 |
| IP Rating | IP54 |
| Operating Temperature | -25°C to +45°C |
| Airframe Material | Fiberglass Composite |
| Redundancy Design | Dual GNSS positioning modules; dual IMUs and dual gyroscopes built into the flight controller |
| Telemetry Range (km) | 15/30/50 km (customizable) |
| Differential System | RTK/PPK |
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