Sukhoi S-37
Sukhoi S-37 | |
---|---|
Type: | Multipurpose fighter |
Design country: | |
Manufacturer: | |
First flight: |
Never happened |
Commissioning: |
Development canceled in 1992 |
Production time: |
Was never produced |
Number of pieces: |
0 |
The Sukhoi S-37 ( Russian Сухой С-37 ) was a project for a single-engine multi-role fighter aircraft based on the Su-27 . The collapse of the Soviet Union prevented the realization.
The name Suchoi S-37 was later used for the Su-47 Berkut .
description
Development of the S-37 probably began in the late 1980s after the single-engine variant of the MiG-29 had failed ( Project R-33 ). Since large parts of the Soviet air force were still equipped with MiG-21 and MiG-23 , there was a need for replacement. The newest fighter aircraft available at the time were the MiG-29 and Su-27. Since both models were too expensive to produce in the required quantities, Sukhoi suggested a single-engine variant of the Su-27. The S-37 was to use the AL-41F engine, which was still in the early conception phase, and which was later used on the MiG 1.44 . Compared to the Su-27, the S-37 had significantly shortened dimensions, with large parts of the wings being redesigned. At the same time, canards and a simple vertical stabilizer were used. With the collapse of the Soviet Union, the S-37 was abandoned. Considerations to finish the machine for the export market failed because of the financing.
Technical specifications
Parameter | Data |
---|---|
Length: | 17.50 m |
Span: | 11.80 m |
Wing area | 50 m² |
Wing extension : | 2.78 |
Wing loading : | 265 kg / m² (at maximum take-off weight) |
Maximum take-off weight: | 25,000 kg |
Top speed: | Mach 1.5 (at optimal height) |
Service ceiling : | 17,000 m |
Range: | approx. 1,500 km |
Crew: | 1 pilot |
Armament: | approx. 8,000 kg external weapon load |
Engine: | A Saturn / Ljulka AL-41F turbofan engine |
Thrust: | 178.45 kN (with afterburner) |
Thrust-to-weight ratio : | 0.73 (at maximum takeoff weight) |