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J-11 (Flanker-L) Chinese Air Superiority Fighter

J-11

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Basic Information
Name
J-11 (Flanker-L) Chinese Air Superiority Fighter
Designation
J-11
Alternate Designation
Equipment Type
Manufacturer
Shenyang Aircraft Corporation
Date of Introduction
1998
Description

The J-11 was finally born in 1998 as a Chinese version of the Soviet-designed Sukhoi Su-27SK air superiority fighter after China secured a $US2.5 billion production agreement which licensed China to build 200 Su-27SK aircraft using Russian-supplied kits. Under the terms of the agreement, these aircraft would be outfitted with Russian avionics, radars and engines. However, in 2004, Russian media reported that Shenyang co-production of the basic J-11 was halted after around 100 examples were built. The PLAAF later revealed a mock-up of an upgraded multi-role version of the J-11 in mid-2002. The indigenous J-11B variant incorporates various Chinese material modifications and upgrades to the airframe with improved manufacturing methods in addition to the inclusion of domestic Chinese technologies such as radar, avionics suites and weaponry, including anti-ship and PL-12 air-to-air missiles presumably for the role of a maritime strike aircraft. The alleged reason for the sudden stop in the production line of the J-11 was because it could no longer satisfy the PLAAF's requirements, due to elements such as the obsolete avionics and radar, which were structured for aerial missions. The J-11/J-11B's legitimacy remains unproven, despite a wealth of information coming to light since 2007. In the course of a press conference at the 2009 Farnborough Airshow, Alexander Fomin, Deputy Director of Russia's Federal Service for Military-Technical Co-operation, reported that Russia had not so far tabled any questions to China with regard to "copying" military equipment. Fomin reported that Russia handed China the licences to manufacture the aircraft and its components, including an agreement on the production of intellectual property rights. Details of intellectual property rights, however have not been disclosed, fuelling speculation about a "secret" contract or parts of the original contract. The licence, at least officially, did not include an aircraft carrier version- Sukhoi Su-33 nor any variant of it, such as the Shenyang J-15. At the MAKS 2009, Rosoboron export's General Manager Anatoli Isaykin was quoted saying: "Russia is going to investigate the J-11B, as a Chinese copy of the Su-27 and Sukhoi Company is partaking in the process." In 2010, Rosoboronexport announced via their official website that it was in talks with the Chinese side, regarding the ongoing production of weapons that Russia considers as unlicensed. In light of the ongoing investigations, Rosoboronexport expressed its concern over future sales of advanced Russian systems and components to China. At the Zhuhai 2002 airshow, a photo was released allegedly depicting a J-11 modified for flight testing of a single WS-10 Taihang turbofan. Andrei Chang, a military specialist on China reported that one J-11A was outfitted with the indigenously produced WS-10A turbofan engine, J-11B also uses WS-10A. However, Russian media reports also indicate that China still intends to upgrade the current J-11 fleet's engines with either Saturn-Lyulka or Salyut powerplants. Engines under consideration include the Saturn AL-31-117S (a development of the Lyulka AL-31F planned for the Russo-Indian Su-30MKIs), and the Salyut AL-31F-M1, an improved variant of the AL-31F engine. In 2002, Russian media reported that Shenyang Aircraft Corporation was looking into replacing Russian-made J-11/Su-27SK components with domestic, Chinese-made parts. Specifically, to replace the Russian-made NIIP N001 radar with a Chinese-made fire control radar based on the Type 147X/KLJ-X family, the AL-31F engine with WS-10A, and Russian R-77 AAM's with Chinese-made PL-9 and PL-12 AAM's. One J-11 was photographed with an AL-31F and a WS-10A engine installed for testing in 2002. However, it was not until 2007 when the Chinese government finally revealed information on the domestic J-11: the J-11 used to test WS-10 was designated as J-11WS, and it was when state television station CCTV-7 aired J-11B footages in mid-2007 when the existence of J-11 with domestic components was finally confirmed officially. Serial manufacturing of the WS-10 and integration with the J-11, proved to be more difficult than expected. As a result, even though several related prototypes had been tested and at least one regiment converted to the Taihang powered J-11B version in 2007, these aircraft were later grounded for an extended period due to a poor operational reliability. A report in the Washington Times suggested that the Chinese engines lasted 30 hours before they needed servicing, compared to 400 hours for the Russian versions. Defects were traced back to the engine manufacturer, Shenyang Liming Aircraft Engine Company employing sub-standard manufacturing and quality control procedures. Several subsequent batches temporarily reverted to the original, Russian AL-31F turbofans. The engines manufacturing problems had finally been solved by the end of 2009 and the WS-10A had reportedly proved mature enough to power the Block 02 aircraft.

Air & Air Defense Specifications
Crew 1
Max Speed 2.1 km/h
Range 3530.0 km
Service Ceiling 9000 m
Variants
J-11A Chinese/Russian assembled Su-27SK from Russian-made kits. 104 were built. They were later upgraded with MAWS. Unconfirmed upgrades include improved cockpit displays, and fire control systems for R-77 or PL-10 missiles. It is also called J-11.
J-11B Indigenously-produced version using Chinese technology, and the first J-11 variant to use the WS-10A turbofan. The airframe is slightly lighter due to greater use of composites. It has new avionics, a glass cockpit, MAWS, and onboard oxygen generator system. Upgrading to AESA radar may have been planned. Photos of China's latest, very long range PL-15 missile on a J-11B may well indicate the undergoing upgrades of AESA radar to the aircraft. More recently aircraft have been spotted with light grey radomes which may indicate ongoing upgrades.
J-11BS A twin-seat version of the J-11B. In 2012, the number of J-11B and J-11BS in service was over 120.
J-11BH Naval version of the J-11B. It was first sighted in May 2010.
J-11BSH Naval version of the J-11BS.
J-15 Carrier-based version based on the J-11B, incorporating structural elements from the Sukhoi Su-33 prototype purchased from Ukraine in 2001. It uses avionics from the J-11B.
J-16 Twin-seat strike fighter based on Russian Sukhoi Su-30MKK sold to China in 2000.[33] A further development of the J-11BS.
J-11D Variant with fixed electronically scanned array radar, IRST, and capability to fire heavier imaging/infrared (IIR) air-to-air missiles. The airframe utilizes composite materials more extensively, particularly in the engine intakes, for improved radar observability. The wings have three hardpoints each. Unconfirmed reports claim it has a new fly-by-wire control system, a glass cockpit, improved EW systems, and an improved version of the WS-10A engine.
System
Alternate Designation(s) J-11 (Flanker-L)
Primary Function / Type Air Superiority Fighter
Manufacturer Shenyang Aircraft Corporation
Crew 1
Number of Engines 2
Number of Hard Points 0: 2 under fuselage, 2 under air ducts, 4 under wings, 2 on wingtips with provisions to carry combinations of: Missiles: PL-12; PL-9; PL-8; Vympel R-77; Vympel R-27; Vympel R-73
Dimensions
Length 21.9 m
Width (Wing Span) 14.7 m
Height 5.92 m
Wing Area 52.84 m2
Empty Weight 16,380 kg
Gross Weight 23,926 kg
Max Takeoff Weight 33,000 kg
Fuel Capacity, Internal Fuel Tank 9,400 kg
Automotive
Engine Name 2 × Lyulka AL-31F or afterburning turbofan engines
Number of Engines 2
Engine Power 75.22 / 123 kN (16,910 / 27,650 lbf) dry / afterburning
Maximum Range 3,530 km
Maximum Speed Mach 2.1
Service Ceiling 9,000 m
Combat Range 1,500 km
G Limits +9
Rate of Climb 300 m/s
Main Gun System
System
Name Gryazev-Shipunov GSh-30-1
Type Autocannon
Caliber 30 mm
Length 1,978 mm
Barrel Length 1,500 mm
Width 156 mm
Height 185 mm
Weight 46 kg
Barrels 1
Action Short recoil operated
Rate of Fire 1,800 rounds/min
Muzzle Velocity 900 m/s
Maximum Firing Range 1,800m
Effective Firing Range 200-1,800m
Ammunition
Type Autocannon
Caliber 30mm
Shell 30×165mm
Basic Load 150 Rounds
Missile Systems
Missile Options PL-12 PL-9 PL-8 Vympel R-77 Vympel R-27 Vympel R-73
Main Missile System #1
Name PL-9
Type Air-to-Air Missile
Length 2.9m
Diameter 0.157m
Wingspan 0.856m
Weight 115kg
Warhead 11.8kg blast-frag, or expanding rod (RF-fuse)
Detonation Mechanism laser proximity fuse
Engine Solid-fuel rocket
Operational Range 22km
Flight Altitude 4.5km
Maximum Speed Mach 2.0
Guidance System multi-element infrared
Rocket Weapon Systems
Note Unguided rocket launcher
Bomb Weapon Systems
Note Free-fall cluster bombs
Fire Control / Avionics
Fire Control Radar NIIP Tikhomirov N001VE Myech coherent pulse Doppler radar. J-11B to be equipped with AESA radar.
Laser Desingator INA
Optic System OEPS-27 electro-optic system
HUD NSts-27 helmet-mounted sight (HMS)
ECM Gardeniya ECM pods
Protection
Stealth Properties No
Heat Signature Reduction INA
Add on Armor INA
NBC Protection Yes
EW Counter Measures Yes
Chaffs/Flares INA
Details
Country of Origin China
Category Fixed Wing Aircraft
Air > Fixed Wing Aircraft
Filter Label
J
Classification
Domain
Air & Air Defense
Equipment Status
Active
Dimensions
Length
21.9 m
Width
14.7 m
Height
5.92 m
Weight
23926 kg
Operators (1)
China
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