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Falcon-1800DH Chinese Unmanned Aerial Vehicle (UAV)

Falcon-1800DH

Tactical Unmanned Aerial Vehicle (UAV)
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Basic Information
Name
Falcon-1800DH Chinese Unmanned Aerial Vehicle (UAV)
Designation
Falcon-1800DH
Alternate Designation
Falcon-1800DH
Equipment Type
Tactical Unmanned Aerial Vehicle (UAV)
Manufacturer
Zhuhai Tianqing Aerospace Technology Co Ltd
Date of Introduction
2024
Description

The Falcon-1800DH is a Chinese unmanned aerial vehicle (UAV) that can be made operational from a packed state in just 30 minutes. It features a modular design, allowing assembly in the field without special tools, which can be accomplished by a crew of four in approximately 15 minutes. This UAV has a composite fuselage and shoulder-mounted, high-aspect-ratio tapered wings equipped with winglets. It also features twin tailbooms that extend from the inner wing sections, culminating in an inverted ‘V-tail.’ The Falcon-1800DH is designed with a tricycle landing gear arrangement, consisting of a retractable nose wheel and a fixed main undercarriage with wheel spats. Additionally, the UAV is equipped with four external hardpoints under its wings—two on each side—for carrying sensors and armament. A single Falcon-1800DH can be transported in a 20-foot general-purpose container.

Air & Air Defense Specifications
Engine 2× piston engines equipped in a push-and-pull configuration, with each engine driving a three-blade propeller.
Max Speed 151.0 km/h
Range 6500.0 km
Endurance 45.00 hrs
Service Ceiling 10000 m
Wingspan 18.60 m
Payload Capacity 700 kg
System
Alternate Designation Falcon-1800DH
Type Unmanned Aerial Vehicle (UAV)
Manufacturer Zhuhai Tianqing Aerospace Technology Co Ltd
Payload Capacity 700 kg
Mission Payload The Falcon-1800DH can be integrated with varied payloads depending on the mission requirements, including armament.
Hardpoints The Falcon-1800DH has four external hardpoints under its wings (two on each) for the carriage of sensors and armament payloads.
Launch Conventional, autonomous wheeled take-off.
Recovery Conventional, autonomous wheeled landing.
Dimensions
Length INA
Height INA
Wingspan 18.6 m
Maximum Takeoff Weight 1,800 kg
Automotive
Engine Name INA
Engine Type 2× piston engines equipped in a push-and-pull configuration, with each engine driving a three-blade propeller.
Engine Power INA
Maximum Speed 151 kt (280 km/h)
Maximum Range 6,500 km
Takeoff Run 500 m
Landing Run 500 m
Service Ceiling 10,000 m
Endurance 45 hours
Details
Country of Origin China
Category UAVs
Air > UAVs
Filter Label
F
Classification
Domain
Air & Air Defense
Equipment Status
Active
Dimensions
Length
Width
18.6 m
Height
Weight
1800 kg
Operators (1)
China
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