Practical and efficient
The assembly, disassembly, and launch process is streamlined, featuring long endurance, flexible deployment, strong scalability, and low fuel consumption.
Fixed-wing unmanned aerial vehicle
GHQ-400
The GHQ-400 unmanned aerial vehicle employs a conventional aerodynamic configuration, featuring a high‑aspect‑ratio midwing and a V‑t tail. A rear‑propeller, two‑cylinder, two‑stroke piston engine provides thrust. The UAV utilizes a tricycle wheeled landing gear for takeoff and landing, meeting the requirements for rapid deployment from rudimentary airfields and low‑cost recoverability. The platform boasts substantial payload capacity, capable of accommodating electro‑optical pods, SAR radar, and other reconnaissance payloads, as well as precision‑guided munitions, enabling it to perform a wide range of mission scenarios.
Technical Features
TECHNICAL FEATURES
-
![Practical and efficient]()
-
![Easy to operate]()
Easy to operate
It integrates a dedicated flight control and navigation system, enabling one‑button takeoff and landing and fully autonomous flight throughout the mission; operators can execute flight plans after minimal training.
Low takeoff and landing requirements
Short‑distance taxiing for takeoff and landing places minimal demands on the runway.
Strong load-carrying capability
It can carry a variety of payload platforms and perform diverse flight missions.
Collaborative capability
Supports one-stop multi-device operation and offers the capability to scale up collaborative tasks across multiple devices.
Performance Parameters
PERFORMANCE PARAMETERS
-
Practical ceiling (altitude)
>5000m
-
Flight altitude (elevation)
500-3000m
-
Cruise speed
130-180 km/h
-
Maximum flight speed
200 km/h
-
Endurance (with 5% fuel remaining upon landing)
15:00, 150 kg of fuel (at an altitude of 2,000 m, at a speed of ≤150 km/h)
-
Takeoff and landing run distance
≯600m (At an elevation of 1,100 m, takeoff and landing on a hard, flat surface with a gradient of ≯3%)
-
Wind resistance during takeoff and landing
It can take off and land in crosswinds of 7 m/s or greater and withstand continuous winds of 15 m/s or more in flight.
-
Mission Equipment Power Supply Capability
1.3 kW
-
Communication Capability (Line-of-Sight Communication)
80 km (Standard configuration, upgradeable upon request)
-
Horizontal and vertical positioning accuracy
All are better than 10 m (RMS)
-
Mission payload capacity
≮60kg
-
Flight life
<500 flight hours
-
Number of takeoffs and landings
<100 times
-
The aircraft features rapid assembly and disassembly capabilities; assembly/disassembly time.
≯30 min (4 people, 1 aircraft)
Load Configuration
LOAD CONFIGURATION
- Airborne communication base station
Application Scenarios
APPLICATION SCENARIOS
Artificial weather modification
Logistics and Transportation Support
