Entry Into service
2013-12-01
Maximum Take-Off Weight
33 t (paragliders: kg)
Pictures
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Aircraft Weight Variants
| Aircraft |
Maximum Take-Off Weight (t (paragliders: kg)) |
Maximum Range (km) |
|
Shenyang J-15 |
33 |
3500 |
Similar airplanes
All data (24 fields)
- Name
- Shenyang J-15
- Manufacturer
- Shenyang Aircraft Corporation
- Description
- The Shenyang J-15 (), also known as Feisha (; NATO reporting name: Flanker-X2, Flanker-K) is a Chinese all-weather, twin-engine, carrier-based 4.5 generation multirole fighter aircraft developed by the Shenyang Aircraft Corporation (SAC) and the 601 Institute, specifically for the People's Liberati…
- First Flight
- 2009-08-31
- Entry Into service
- 2013-12-01
- Designer
- Shenyang Aircraft Corporation
- Length (m)
- 22.28
- Height (m)
- 5.92
- Cockpit Crew
- 1
- Max Speed (km/h)
- 2300
- Max Ceiling (m)
- 18000
- Rate of Climb (m/s)
- 246
- Armament
- 1 × 30 mm GSh-30-1 cannon with 150 rounds; Munitions on twelve external hardpoints with a capacity of 6,500 kg, including:; PL-15 long-range air-to-air missile (J-15T and J-15D); PL-12 medium-range air-to-air missile; PL-10 short-range air-to-air missile; PL-8 short-range air-to-air missile ; YJ-83K anti-ship cruise missile; YJ-15 anti-ship cruise missile; KD-88 standoff land attack missile; AKF-…
- Max Mach (Mach)
- 2.17
- National Origin
- China
- Number Built
- 116
- Powerplant Description
- 2 × Saturn AL-31 or WS-10B afterburning turbofans
- Primary Users
- People's Liberation Army Naval Air Force
- Status
- In service / In production
- Wikipedia Article (URL)
- en.wikipedia.org/wiki/Shenyang_J-15
- Flat Wing Span (m)
- 14.7
- Flat Wing Area (m²)
- 67.84
- Aircraft Engine
- Saturn AL-31
- Number of Engines
- 2