Sukhoi Su-33

Airplanes

Length

21.19 m

Flat Wing Span

14.7 m

Height

5.93 m

Flat Wing Area

67.84 m²

Max Speed

2300 km/h

Max Mach

2.17 Mach

Max Ceiling

17000 m

Number of Engines

Aircraft Engine

First Flight

1987-08-17

Entry Into service

1998-08-31

Number Built

Maximum Take-Off Weight

33 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-33	33	3000

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)
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
Sukhoi Su-37		21.935	14.698	Compare
Sukhoi Su-30		21.935	14.7	Compare
Shenyang J-16	Shenyang WS-10	21.9	14.7	Compare

All data (29 fields)

Name: Sukhoi Su-33
Manufacturer: Sukhoi Civil Aircraft
Description: The Sukhoi Su-33 (-33; NATO reporting name: Flanker-D) is a Soviet/Russian all-weather carrier-based twin-engine air superiority-focused multirole fighter designed by Sukhoi and manufactured by Komsomolsk-on-Amur Aircraft Production Association.
ICAO Code: SU27
First Flight: 1987-08-17
Entry Into service: 1998-08-31
Production End: 1999-01-01
Designer: Sukhoi Civil Aircraft
Type: Carrier-based air superiority fighter with multirole capabilities
Length (m): 21.19
Height (m): 5.93
Cockpit Crew: 1
Max Speed (km/h): 2300
Min Speed (km/h): 240
Max Ceiling (m): 17000
Rate of Climb (m/s): 246
Armament: 1 × 30 mm Gryazev-Shipunov GSh-30-1 autocannon with 150 rounds; 12 × external hardpoints
Max Mach (Mach): 2.17
National Origin: Soviet Union
Number Built: 24
Powerplant Description: 2 × Saturn AL-31F3 afterburning turbofan engines, 74.5 kN thrust each
Primary Users: Russian Navy
Status: In service
Wikipedia Article (URL): en.wikipedia.org/wiki/Sukhoi_Su-33
Flat Wing Span (m): 14.7
Flat Wing Area (m²): 67.84
Wake Category: M
Aircraft Engine: Saturn AL-31
Number of Engines: 2