Sukhoi Su-27

Airplanes

Length

21.9 m

Flat Wing Span

14.7 m

Height

5.92 m

Flat Wing Area

62 m²

Max Speed

2500 km/h

Max Mach

2.35 Mach

Max Ceiling

18500 m

Number of Engines

First Flight

1977-05-20

Entry Into service

1985-06-22

Number Built

680

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)
Sukhoi Su-27	33	3530

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)
Shenyang J-11		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 (26 fields)

Name: Sukhoi Su-27
Manufacturer: Sukhoi Civil Aircraft
Description: The Sukhoi Su-27 (; NATO reporting name: Flanker) is a Soviet twin-engine supersonic supermaneuverable fighter aircraft designed by Sukhoi.
ICAO Code: SU27
First Flight: 1977-05-20
Entry Into service: 1985-06-22
Production End: 2010-01-01
Designer: Sukhoi Civil Aircraft
Length (m): 21.9
Height (m): 5.92
Cockpit Crew: 1
Max Speed (km/h): 2500
Max Ceiling (m): 18500
Rate of Climb (m/s): 300
Armament: 1 × 30 mm Gryazev-Shipunov GSh-30-1 autocannon with 150 rounds; 10 external pylons
Max Mach (Mach): 2.35
National Origin: Soviet Union
Number Built: 680
Powerplant Description: 2 × Saturn AL-31F afterburning turbofan engines, 75.22 kN thrust each
Primary Users: Russian Aerospace Forces, People's Liberation Army Air Force , Uzbekistan Air and Air Defence Forces , See Operators section for others
Status: In service
Wikipedia Article (URL): en.wikipedia.org/wiki/Sukhoi_Su-27
Flat Wing Span (m): 14.7
Flat Wing Area (m²): 62
Wake Category: M
Number of Engines: 2