Sukhoi Su-30

Airplanes

Length

21.935 m

Flat Wing Span

14.7 m

Height

6.36 m

Flat Wing Area

62 m²

Max Speed

2120 km/h

Max Mach

2 Mach

Max Ceiling

17300 m

Number of Engines

First Flight

1989-12-31

Entry Into service

1992-01-01

Number Built

630

Maximum Take-Off Weight

34.5 t (paragliders: kg)

Maximum Range

3000 km

Pictures

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Aircraft	Maximum Take-Off Weight (t (paragliders: kg))	Maximum Range (km)
Sukhoi Su-30	34.5	3000

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)
Sukhoi Su-37		21.935	14.698	Compare
Shenyang J-16	Shenyang WS-10	21.9	14.7	Compare
Sukhoi Su-35		21.9	15.3	Compare
Shenyang J-11		21.9	14.7	Compare
Sukhoi Su-27		21.9	14.7	Compare
Shenyang J-15	Saturn AL-31	22.28	14.7	Compare

All data (26 fields)

Name: Sukhoi Su-30
Manufacturer: Sukhoi Civil Aircraft
Description: The Sukhoi Su-30 (; NATO reporting name: Flanker-C/G/H) is a twin-engine, two-seat supermaneuverable fighter aircraft developed in the Soviet Union in the 1980s by Russia's Sukhoi Aviation Corporation.
ICAO Code: SU27
First Flight: 1989-12-31
Entry Into service: 1992-01-01
Designer: Sukhoi Civil Aircraft
Type: Multirole fighter
Length (m): 21.935
Height (m): 6.36
Cockpit Crew: 2
Max Speed (km/h): 2120
Max Ceiling (m): 17300
Rate of Climb (m/s): 230
Armament: 1 × 30 mm Gryazev-Shipunov GSh-30-1 autocannon with 150 rounds; 12 hardpoints
Max Mach (Mach): 2
National Origin: Soviet Union
Number Built: 630
Powerplant Description: 2 × Saturn AL-31FL/FP Afterburning turbofan engines, 74.5 kN thrust each
Primary Users: Russian Aerospace Forces, Indian Air Force , People's Liberation Army Air Force , Algerian Air Force
Status: In service
Wikipedia Article (URL): en.wikipedia.org/wiki/Sukhoi_Su-30
Flat Wing Span (m): 14.7
Flat Wing Area (m²): 62
Wake Category: M
Number of Engines: 2