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J-15 (Flanker-X2) Chinese Carrier-Based Air Superiority Fighter

J-15

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Basic Information
Name
J-15 (Flanker-X2) Chinese Carrier-Based Air Superiority Fighter
Designation
J-15
Alternate Designation
Equipment Type
Manufacturer
Shenyang Aircraft Corporation
Date of Introduction
2013
Description

The Shenyang J-15, NATO reporting name: Flanker-X2, also known as Flying Shark, is a 4th generation, twin-jet, all-weather, carrier-based fighter aircraft in development by the Shenyang Aircraft Corporation and the 601 Institute for the Chinese People's Liberation Army Navy's aircraft carriers. It is developed from J-11B as well as from studying a prototype of Su-33. An unfinished Su-33 prototype, the T-10K-3, was acquired from Ukraine in 2001 and is said to have been studied extensively, and reverse engineered, with development on the J-15 beginning immediately afterward. While the J-15 appears to be structurally based on the prototype of the Su-33, the indigenous fighter features Chinese technologies as well as avionics from the J-11B program. In February 2018, discussions about replacing the aircraft appeared in several Chinese media outlets including Xinhua and China's main military newspaper, discussing that it belongs to the 4th or 4.5 generation fighters. Thus, the J-15 is viewed as an interim carrier-based fighter until a 5th-generation successor enters service, one that may be based on the J-20 or J-31.

Air & Air Defense Specifications
Crew 1
Engine Afterburning Turbofan (132 hp)
Max Speed 2409.0 km/h
Range 3000.0 km
Wingspan 14.70 m
Variants
J-15 Single-seat variant.
J-15B Updated variant.
J-15S Two-seat variant, first flown in 2012.
J-15D Two-seat variant with EW pods and other electronic equipment installed and IRST sensor removed. Begun operational testing in December 2018.
System
Alternate Designation(s) J-15; NATO: Flanker-X2
Primary Function / Type This carrier-capable aircraft is intended for air-superiority, air-defense and anti-ship missions.
Manufacturer Shenyang Aircraft Corporation
Crew 1 (pilot)
Number of Engines 2 ea
Number of Hard Points 12 × external hardpoints with a capacity of up to 6,500 kg (14,300 lb) of ordnance, with provisions to carry combinations of Rockets, Missiles, and Bombs.
Dimensions
Length 12.19 m without probe
Wingspan 14.70 m
Wingspan Folded 7.40 m
Height 5.85 m
Wing Area 67.80 m sq
Wheelbase 5.87 m
Wheel Track 4.40 m
Empty Weight 18,500 kg
Normal Takeoff Weight 25,000 kg
Maximum Takeoff Weight 29,940 kg
Maximum Weight 33,000 kg after in-flight refueling
Maximum Combat Load 6,500 kg
Automotive
Engine Name 2 × Shenyang WS-10
Number of Engines 2 ea
Engine Type Afterburning Turbofan
Engine Power 132 kN (30,000 lbf) thrust each
Fuel Capacity 20,944 lb (9,500 kg) internal
Maximum Speed 2,409 km/h
Maximum Speed at Sea Level 1,400 km/h
Approach Speed 240 km/h
Maximum Range 3,000 km w/out refueling
Ceiling 17,000 m
Carrier Takeoff 120 m on 14-deg ramp
Carrier Landing 90 m with arrestor hook
Maximum Load +9 G
Operational Load +8 G
Main Gun System
System
Name Gryazev-Shipunov GSh-30-1
Type Autocannon
Caliber 30 mm
Length Gryazev-Shipunov GSh-30-1
Barrel Length 1,500 mm
Width 156 mm
Height 185 mm
Weight 46 kg
Barrels 1 ea
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 Rifle
Caliber 30 mm
Shell 30×165mm
Basic Load 150 Rounds
Missile Systems
Anti-Air Missiles AA-10 Alamo, AA-8 Aphid, AA-11 Archer, AA-12 Adder AAMs
Anti-Ship Missiles AS-17 Krypton, Moskit ASM-MSS (SS-N-22 Sunburn)
Anti-Ship Missile
Name P-270 Moskit
Type Supersonic Anti-Ship Cruise Missile
Manufacturer MKB Raduga
Length 9.745 m
Diameter 0.8 m
Wingspan 2.10 m
Weight 4,500 kg
Warhead Weight 300 KG (660 lb) overall 150 kg (330 lb) explosive or 120 kt of TNT fission-fusion thermonuclear weapon
Engine Four ramjets (solid fuel rocket on air-to-surface version)
Operational Range 120–250 km
Flight Altitude 20 m (66 ft) above sea level
Maximum Speed Mach 3 (3,675 km/h)
Guidance System Inertial guidance plus terminal active radar homing
Rockets
Note S-8, S-13 or S-25 pods
Bombs
Note up to 8 x 1,100 lb (500 kg) or 28 x 550 lb (250 kg)
Fire Control / Avionics
Fire Control Radar NIIP N011 multi-mode look-down shoot-down; or Phazotron Zhuk-27
Navigation Radar INA
Protection
Stealth Properties None
Heat Signature Reduction INA
NBC Protection INA
EW Counter Measures INA
Chaffs/Flares Yes
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
12.19 m
Width
Height
5.85 m
Weight
25000 kg
Operators (2)
Russia
China
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