Shenyang J-11

Airplanes

Length

21.9 m

Flat Wing Span

14.7 m

Height

5.92 m

Flat Wing Area

52.84 m²

Max Mach

2.35 Mach

Max Ceiling

18500 m

Number of Engines

First Flight

1998-01-01

Entry Into service

1998-01-01

Number Built

440

Maximum Take-Off Weight

33 t (paragliders: kg)

Maximum Range

3530 km

Pictures

No pictures yet for this family.

Aircraft	Maximum Take-Off Weight (t (paragliders: kg))	Maximum Range (km)
Shenyang J-11	33	3530

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)
Sukhoi Su-27		21.9	14.7	Compare
Shenyang J-15	Saturn AL-31	22.28	14.7	Compare
Sukhoi Su-37		21.935	14.698	Compare
Sukhoi Su-33	Saturn AL-31	21.19	14.7	Compare
Sukhoi Su-30		21.935	14.7	Compare
Shenyang J-16	Shenyang WS-10	21.9	14.7	Compare

All data (24 fields)

Name: Shenyang J-11
Manufacturer: Shenyang Aircraft Corporation
Description: The Shenyang J-11 (Chinese: 歼-11; NATO reporting name: Flanker-B+/Flanker-L), also known as Yinglong () is a 4th generation twin-engine jet fighter of the People's Republic of China derived from the Soviet-designed Sukhoi Su-27SK.
ICAO Code: SU27
First Flight: 1998-01-01
Entry Into service: 1998-01-01
Designer: Shenyang Aircraft Corporation
Type: Air superiority fighter
Length (m): 21.9
Height (m): 5.92
Cockpit Crew: 1
Max Ceiling (m): 18500
Armament: 1× 30 mm (1.18 in) Gryazev-Shipunov GSh-30-1 cannon with 150 rounds; Free-fall cluster bombs; Unguided rocket launcher; 10: 2 under fuselage, 2 under air ducts, 4 under wings, 2 on wingtips
Max Mach (Mach): 2.35
National Origin: China
Number Built: 440
Powerplant Description: 2 × Shenyang WS-10A "Taihang" afterburning turbofans, 132 kN thrust each
Primary Users: People's Liberation Army Air Force
Status: In active service
Wikipedia Article (URL): en.wikipedia.org/wiki/Shenyang_J-11
Flat Wing Span (m): 14.7
Flat Wing Area (m²): 52.84
Wake Category: M
Number of Engines: 2