The ZF200P is a small long-endurance runway takeoff and landing fixed-wing UAV.
It takes off and lands on a runway, suited for routine operations where a runway is available.
It has a wingspan of 6660 mm, a fuselage length of 3850 mm, a height of 1320 mm, an empty weight of 85 kg, a maximum takeoff weight of 200 kg, a maximum payload of 100 kg and a fuel tank capacity of 60 L.
The fuel tail-push power system with built-in electric start delivers an endurance of 180 minutes and a maximum range of 390 km.
Its service ceiling reaches 6000 m, with a maximum speed of 160 km/h and a cruise speed of 110-150 km/h.
The climb rate is <=3.5 m/s and the descent rate is <=1.5 m/s.
It withstands level-5 winds in the VTOL phase and level-6 winds in the cruise phase, with an IP54 rating and an operating temperature range of -10°C to +45°C.
The airframe is built of fiberglass composite for durability.
The airframe stows to 3440x1290x910 mm for easy transport and rapid deployment.
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 heavy payload delivery and inspection.


ZF200P Small Long-Endurance Runway Takeoff & Landing Fixed-Wing UAV, 180 min Endurance, 390 km Range
The ZF200P is a small long-endurance runway takeoff and landing fixed-wing UAV with fuel tail-push propulsion, a 200 kg MTOW, a 100 kg payload and a 60 L fuel tank, 180 minutes of endurance and a 390 km range; its fiberglass composite airframe and RTK/PPK support make it ideal for heavy-payload delivery.
Original price was: $51,400.00.$40,100.00Current price is: $40,100.00.
| Product Positioning | Small Long-Endurance |
|---|---|
| Takeoff/Landing Mode | Runway Takeoff & Landing |
| Power System | Fuel-Powered |
| Start Mode | Built-In Electric Start |
| Cruise Power | Fuel Tail-Push Propeller |
| Wingspan (mm) | 6660 |
| Fuselage Length (mm) | 3850 |
| Height (mm) | 1320 |
| MTOW (kg) | 200 |
| Empty Weight (kg) | 85 |
| Max Payload (kg) | 100 |
| Fuel Tank Capacity (L) | 60 |
| Endurance | 180 min |
| Max Range (km) | 390 |
| Service Ceiling (m) | 6000 |
| Max Speed (km/h) | 160 |
| Cruise Speed (km/h) | 110-150 |
| Climb Rate (m/s) | <=3.5 |
| Descent Rate (m/s) | <=1.5 |
| Wind Resistance | Level 5 (VTOL Phase) / Level 6 (Cruise Phase) |
| IP Rating | IP54 |
| Operating Temperature | -10°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 |
| Stowed Size (mm) | 3440x1290x910 |
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