සාරාංශය
The Sukhoi Su-37 was a single-seat twin-engine aircraft designed by the Sukhoi Design Bureau which served as a technology demonstrator. It met the need to enhance pilot control of the Su-27M, a further development of the Su-27. The sole example built was originally the eleventh Su-27M (T10M-11) built by the Komsomolsk-on-Amur Aircraft Production Association before having thrust-vectoring nozzles installed. It also had updated flight- and weapons-control systems. The aircraft made its maiden flight in April 1996. Throughout the flight-test program, the Su-37 demonstrated its supermaneuverability at air shows, performing manoeuvres such as a 360-degree somersault. The aircraft crashed in December 2002 due to structural failure. The Su-37 did not enter production, despite a report in 1998 which claimed that Sukhoi had built a second Su-37 using the twelfth Su-27M airframe, T10M-11 remained the sole prototype. Sukhoi had instead applied the aircraft's systems to the design bureau's other fighter designs.
පිරිවිතර
මානයන්
| දිග | 21.94 m |
|---|---|
| පියාපත් පළල | 14.70 m |
| උස | 5.93 m |
කාර්ය සාධනය
| පරාසය | 3,300 km |
|---|
බලාගාරය (එන්ජින්)
| එන්ජින් මාදිලිය | Saturn AL-31 |
|---|
සංඛ්යා ප්රසිද්ධ මූලාශ්රවලින් එකතු කළ ඒවා බැවින් ආසන්න අගයන් විය හැක; ප්රභේදය සහ සැකසුම අනුව වෙනස් විය හැක.
ඡායාරූප
ඡායාරූපය 1: Mike Freer / Wikimedia Commons · GFDL 1.2
සමහර පෙළ සහ රූප Wikipedia / Wikimedia Commons වෙතින් CC BY-SA බලපත්ර යටතේ ලබාගෙන ඇත. මූලාශ්රය


