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J-10

J-10

Multi-Role Fighters
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Basic Information
Name
J-10
Designation
J-10
Alternate Designation
Equipment Type
Multi-Role Fighters
Manufacturer
Date of Introduction
Description

The J-10 is a lightweight, single-engine, multi-role fighter developed by Chengdu Aircraft Industry Corporation (CAC) and 611 Institute for the People's Liberation Army Air Force (PLAAF). The high-performance J-10 aircraft has been designed as an air superiority fighter with air-to-surface capability. The aircraft's development started in the mid-1980s based upon the cancelled Israeli Air Force Lavi lightweight fighter. In the 1990s, the Russians joined the J-10 project providing the AL-31FN as the replacement engine for Chinese incapable WS-10 turbofan. The first J-10 prototype made its maiden flight in March 1998 and the aircraft achieved initial operational capability (IOC) with PLAAF by late 2003/early 2004. The J-10 aerodynamic configuration is based on a delta-wing with canard foreplanes design with a single ventral air intake. All in, the J-10 is very similar to Eurofighter/Typhoon multi-role aircraft being procured by European countries. The J-10 aircraft is made of composite materials resulting in a high thrust-to-weight ratio with enhanced maneuverability and low drag thanks to its advanced aerodynamics. The flight control system is based on a 4-channel fly-by-wire (FBW) system. An engine digital control system provides for fuel consumption efficiency. The J-10 has been fitted with a glass cockpit and pulse-Doppler radar system capable of tracking 10 targets at ranges of up 100 km while engaging four of them simultaneously. The J-10 aircraft has 11 external stations for weapons and auxiliary fuel tanks. For air-to-air engagements the aircraft can be equipped with PL-8 (a version of Israel's Python 3) infrared-guided short-range and PL-12 radar active medium-range missiles. Laser guided bombs, free fall bombs and rockets are provided for the air-to-ground attack role. In addition, the J-10 is provided with a single-barrel 23mm internal gun. Future plans call for the installation of the improved Chinese-built WS-10A turbofan in lieu of AL-31FN. The J-10 might be fitted with a detachable air refueling probe to extend its radius of operation or carrying a greater load of weapons. A pilot's helmet-mounted sight system is under study.

Overview (Deagel)
Group Multi-Role Fighters
Status Active
Also Known As F-10A (export name), J-10B (improved version fitted with thrust vectoring AL-31 engine), Jian-10, Vigorous Dragon
Origin China
Contractor Chengdu Aircraft Industry Corporation
Initial Operational Capability (IOC) 2006
First Flight March 22, 1998
Total Production 280
Specifications (Deagel)
Crew 1
External Stations 11
Number of Engines 1
Tracked Aerial Targets 10
Area — Wing Area 39 square meter
Dimensions — Length 15.5 meter
Dimensions — Main Gun Caliber 23 millimeter
Dimensions — Wingspan 9.7 meter
G-load — Max Maneuvering Load Factor 9 g
G-load — Min Maneuvering Load Factor -3.00 g
Mass — Empty Weight 8,300 kilogram
Mass — Fuel Load 4,500 kilogram
Mass — Max Takeoff Thrust 27,557 pound
Mass — Max Takeoff Weight 18,000 kilogram
Mass — Operational Weight 13,200 kilogram
Performance — Radius of Operation 1,100 kilometer
Performance — Take Off Run Distance 500 meter
Speed — Top Speed at High Altitude 2.2 mach
Speed — Top Speed at Sea Level 1.2 mach
Gear (Deagel)
Item 1 Air-to-Air Missiles: PL-12
Item 2 Air-to-Air Missiles: PL-8
Item 3 Bombs: FT-12
Item 4 Bombs: LS-6
Item 5 Bombs: LT-2
Item 6 Fighter Aircraft Engines: AL-31FN (1)
Item 7 Fighter Aircraft Engines: WS-10A (1)
Item 8 Optronic Systems: WMD-7 (1)
Variants
Variant 1 J-10A
Variant 2 J-10S
Variant 3 J-10B
Variant 4 J-10C
Details
Country of Origin China
Category Multirole Aircraft
Air > Multirole Aircraft
Classification
Domain
Air & Air Defense
Equipment Status
Active
Dimensions
Length
Width
Height
Weight
18000 kg
Related Equipment (1)
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