SU-35
The Sukhoi Su-35 is the designation for two improved derivatives of the Su-27 air-defence fighter. They are single-seat, twin-engine, supermaneuverable aircraft, designed by the Sukhoi Design Bureau and built by Sukhoi.
Type
Role
Country of Origin
Introduction
Note
The Sukhoi Su-35 (Russian: Сухой Су-35; NATO reporting name: Flanker-E) is the designation for two improved derivatives of the Su-27 air-defence fighter. They are single-seat, twin-engine, supermaneuverable aircraft, designed by the Sukhoi Design Bureau and built by the Komsomolsk-on-Amur Aircraft Plant.
The type was originally developed by the Soviet Union from the Su-27 and was known as the Su-27M. It incorporated canards and a multi-function radar giving it multi-role capabilities. The first prototype made its maiden flight in June 1988. Following the dissolution of the Soviet Union Sukhoi re-designated it as the Su-35 to attract export orders. Fourteen aircraft were produced and used for tests and demonstrations; one example had thrust-vectoring engines and was in turn redesignated the Su-37. A sole Su-35UB two-seat trainer was also built in the late 1990s that resembled the Su-30MK family.
Crew: 1
Length: 21.9 m
Wingspan: 15.3 m
Height: 5.9 m
Wing area: 62 m2
Airfoil: 5%
Empty weight: 19,000 kg
Gross weight: 25,300 kg with 50% internal fuel
Max takeoff weight: 34,500 kg
Fuel capacity: 11,500 kg internal
Type of packaging
Quantity per pack
Number in a wooden case
Dimensions of a wooden case
Weight of the package
Weight of wooden case
Weight
Volume m3
UN Number
Hazard Class
SU-35
Description
Type
Role
Country of Origin
Introduction
Note
The Sukhoi Su-35 is the designation for two improved derivatives of the Su-27 air-defence fighter. They are single-seat, twin-engine, supermaneuverable aircraft, designed by the Sukhoi Design Bureau and built by Sukhoi.
The Sukhoi Su-35 (Russian: Сухой Су-35; NATO reporting name: Flanker-E) is the designation for two improved derivatives of the Su-27 air-defence fighter. They are single-seat, twin-engine, supermaneuverable aircraft, designed by the Sukhoi Design Bureau and built by the Komsomolsk-on-Amur Aircraft Plant.
The type was originally developed by the Soviet Union from the Su-27 and was known as the Su-27M. It incorporated canards and a multi-function radar giving it multi-role capabilities. The first prototype made its maiden flight in June 1988. Following the dissolution of the Soviet Union Sukhoi re-designated it as the Su-35 to attract export orders. Fourteen aircraft were produced and used for tests and demonstrations; one example had thrust-vectoring engines and was in turn redesignated the Su-37. A sole Su-35UB two-seat trainer was also built in the late 1990s that resembled the Su-30MK family.
Technical data and Packaging
Crew: 1
Length: 21.9 m
Wingspan: 15.3 m
Height: 5.9 m
Wing area: 62 m2
Airfoil: 5%
Empty weight: 19,000 kg
Gross weight: 25,300 kg with 50% internal fuel
Max takeoff weight: 34,500 kg
Fuel capacity: 11,500 kg internal
Type of packaging
Quantity per pack
Number in a wooden case
Dimensions of a wooden case
Weight of the package
Weight of wooden case
Weight
Volume m3
UN Number
Hazard Class
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