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Design organisation Sukhoi Design Office
Main secundary design organisations Motor Building Association and NPO Saturn Research and Production Association
Production organisaton - Komsomolsk-on-Amur Aviation Production Association (KnAAPO)
Primary task Multi-role fighter jet
Type aircraft 4++ generation fighter jet
Length 21.9 meters
Height 5.9 meters
Wingspan 15.3 meters
Wing surface  
Aspect ratio  
Sweep back  
Engines 2x 117S turbofan with afterburner and Trust Vector Control
Thrust 8.800 kgf
14.5000 kgf (with afterburner)
Weight (empty) 25.3000 kgs
Weight (start, maximum, MTOW) 34.500 kg s
Weight (landing, maximum, MLW)  
Required runway length (start)  
Required runway length (landing)  
Cruise speed  
Maximum speed 1400 km/h (MSL)
2400 km/h (high altitude)
Mach 2.25
Ceiling 18.000 meters
Maximum range 1580 km (MSL)
3500 km (high altitude)
1500 km (+ 2 external fuel tanks)
Fuel capacity 11.500 kgs
Air-to-air-refueling capability Yes
Passengers none
Payload none
Armament 30mm boardcanon
Air-to-air missiles
Air-to-ground missiles
Maximum weapon load 8000 kilograms over 12 pylons
Maximum G resistance +9
Radar Irbis-E, passive phased, antenna
Type flight controls  
Landing gear  
Versions Su-35BM
Crew 1 or 2
Overall flight hours 6000 hours
First flight 19 February 2008
First delivery n.a
Operational since n.a
Successor of Su-30MK
Replaced by n.a.
Comparable aircraft Eurofighter Typhoon, Rafale
Operators (current and future) none
Main operators none
Amphibious usage No
Status In development

Su-35 from the Russian Air Force

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Last updated: 18 January 2014