Technical data
Type S-37
Function MFI prototype
Year 1997
Crew 1
Engines 2* D-30F6 or
2*14500kg AL-31FU
Length 22.6m
Wingspan 16.7m
Wing area -
Empty weight 24000kg
Loaded weight -
Wing Load (kg/m2) -
Power load (kg/hp) -
Speed at 0m 1400km/h
Speed at 2500km/h
Turn time -
Landing Speed -
Landing Roll -
Takeoff Roll -
Range 3300km
Ceiling 18000m
Climb
1000m -
3000m -
Armament
Guns ?
Hardpoints 14: 2 on wingtips
6-8 underwing
6-4 conformal underfuselage
Bombs KAB-500/1500
Rockets (AA) R-77; R-77PD; R-73; K-74
Rockets (AS) X-29T; X-29L; X-59M; X-31P/A

S-37 'Berkut', M.Simonov ( Sukhoj Bureau)

courtesy of

The "Berkut" ("Golden Eagle") of 1997 (formerly referenced as S-32) took place of smaller single-engine S-37 project of 1991. It looks like a radical revision of dedicated aircraft line Su-27-Su-37. It has a layout of tandem triplane with forward swept wings and thrust-vectoring engine (equipped with digital control system). This combination provides exceptional maneuverability, what in conjunction with elements of stealth technology and new more powerful engines can provide Russia with a superior aircraft for 20th century.

While forward-swept wings are not a best choice for supersonic performance, while provides great advantages at high angles of incidence and in post-stall maneuvering much needed in close-in dogfight, as well as missile evasion. This approach radically differs from USAF concept of stealth, supercruising and beyond visible range (BVR) combat. RAM coating is chosen for stealth contrary to American F-22 radar absorbing structures (RAS).

The tandem triplane scheme was first tried on T-10-24 prototype for Naval Flanker. Canard foreplanes are used on latest Sukhoj Su-34, Su-32FN, Su-35, Su-37, as well as S-37 and Su-54 projects.

There are several riddles surrounding this aircraft.


Modified January 25, 1998
and ;
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