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

J-11B

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Basic Information
Name
J-11B (Flanker-L) Chinese Air Superiority Fighter
Designation
J-11B
Alternate Designation
Equipment Type
Manufacturer
Shenyang Aircraft Corporation
Date of Introduction
2000
Description

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. The controversial J-11B is an unauthorised derivative of the Sukhoi J-11A/Su-27SK, built by Shenyang in China. The aircraft has been the subject of an ongoing dispute between Beijing and Moscow which has caused the suspension of production of the second batch on indigenously manufactured legally licenced J-11A/Su-27SK. The J-11B is not an exact clone of the Su-27SK, despite the commonly held view this is so. The airframe and engines can be considered to be 'cloned' but the systems are mostly unique to this variant. Known differences include: A Chinese IRST set located in the centreline position as with the OLS-27 in early Su-27S. A planar array multimode radar which resembles the Phazotron Zhuk-27 series. It includes an IFF interrogator array. An Onboard Oxygen Generator System (OBOGS). Only the most recent Russian variants have an OBOGS. A unique glass cockpit design, with an asymmetric layout quite different from the Su-30MKK/MK2 and Su-27SMK. An optical MAWS system claimed to operate in the UV band. Dielectric panels on the stabilators not seen on any Russian variant. The differences between the J-11B, Su-27SK and Su-27SMK are sufficiently great that this must be considered a unique offshoot of the Flanker family of fighters, not a subtype of the baseline Su-27SK/J-11A. Chinese sources claim that the J-11B variant deployed with PLANAF units, such as the 22nd Fighter Regiment, 8th PLAN Fighter Division, is designated the J-11BH. In 2011 images emerged of the prototype of the J-11BS which is an analogue of the Su27UBK, with the PLANAF variant claimed to be the J-11BSH.

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 ariant with fixed electronically scanned array radar, IRST, and capability to fire heavier imaging/infrared (IIR) air-to-air missiles. The airframe makes greater use of composite materials, especially in the engine intakes for lower radar observability. The wings have three hardpoints each. Unconfirmed reports claim it has a new fly-by-wire control system, glass cockpit, improved EW systems, and an improved version of the WS-10A engine.
System
Alternate Designation(s) J-11B (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 × WS-10A turbofan
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
Onboard Oxygen Generator System (OBOGS) An Onboard Oxygen Generator System (OBOGS). Only the most recent Russian variants have an OBOGS.
MAWS System An optical MAWS system claimed to operate in the UV band.
Protection
Stealth Properties No
Heat Signature Reduction INA
Add on Armor INA
Cockpit A unique glass cockpit design, with an asymmetric layout quite different from the Su-30MKK/MK2 and Su-27SMK.
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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