CH-804 Chinese Unmanned Aerial Vehicle (UAV)
CH-804
Tactical Unmanned Aerial Vehicle (UAV)
Other
Basic Information
Name
CH-804 Chinese Unmanned Aerial Vehicle (UAV)
Designation
CH-804
Alternate Designation
CH-804
Equipment Type
Tactical Unmanned Aerial Vehicle (UAV)
Manufacturer
CASC
Date of Introduction
2020
Description
The CH-804 Chinese Unmanned Aerial Vehicle (UAV) is based on the ch-803 UAV system, which optimizes the power system and aerodynamic shape to greatly improve the endurance performance. The ch-804 is a short-range vehicle-mounted unmanned aerial vehicle (UAV) system with features of easy to use, long flight time and high reliability, which can be used for battalion-level day and night air reconnaissance, air surveillance and counter-terrorism operations. It can also be used in such civil fields as environmental monitoring, aerial surveying and mapping, pipeline patrol, urban security and defense, with international advanced level.
Air & Air Defense Specifications
Engine
Gasoline
Max Speed
120.0 km/h
Range
800.0 km
Endurance
8.00 hrs
Service Ceiling
4000 m
Wingspan
4.00 m
Payload Capacity
4 kg
Variants
CH-804C
The CH-804C Chinese Unmanned Aerial Vehicle (UAV) features a slim, conical-shaped fuselage with its wings positioned towards the back in a mid-wing configuration. The aircraft has twin booms that extend beneath the fixed wings on either side, attaching to the underside of each main wing surface. Each tailboom is equipped with two rotors, located at both the front and rear ends. The twin booms end in vertical fins at the back, which are connected at the top by a horizontal surface. The main engine, which drives a two-blade propeller, is installed at the rear of the fuselage.
CH-804D
CH-804D is a variant of CH-804 with twin-boom mounted inverted V-tail and shoulder-mounted wings. The UAV is also fitted with four landing legs (two ahead, and two aft).
System
Alternate Designation
CH-804
Type
Unmanned Aerial Vehicle (UAV)
Manufacturer
China Aerospace Science and Technology Corporation (CASC)
Payload Capacity
4.8 kg
Payload
2-in-1 photoelectric payload/hd camera
Deployment Time
less than 30 min
Launch Method
Catapult
Recovery Method
Parachute
Dimensions
Length
INA
Height
INA
Wingspan
4.0 m
Maximum Takeoff Weight
24.0 kg
Automotive
Engine Name
INA
Engine Type
Gasoline
Engine Power
INA
Maximum Range
800 km
Cruising Speed
90-110 km/h
Maximum Speed
120 km/h
Cruising Altitude
500-1,500 m
Service Ceiling
4,000 m
Endurance
8 hours
Details
Country of Origin
China
Category
UAVs
Air > UAVs
Filter Label
C
Classification
Domain
Air & Air Defense
Equipment Status
Active
Dimensions
Length
—
Width
4 m
Height
—
Weight
24 kg
Operators (1)
China
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