Su-37 Flanker Specifications
| Primary Function: | Air superiority fighter |
| Contractor: | Sukhoi Design Bureau |
| Crew: | One |
| Unit Cost: | N/A |
| Powerplant | |
| Two Lyulka AL-37FU vectored-thrust afterburning turbofans, 30,855 lb thrust each | |
| Dimensions | |
| Length: | 21.94 m (72 ft) |
| Wingspan: | 15.16 m (49 ft 9 in) |
| Height: | 6.84 m (22 ft 5 in) |
| Weights | |
| Empty: | N/A |
| Maximum Takeoff: | 34,000 kg (74,960 lbs) |
| Performance | |
| Speed: | 2,500 km/h (1,553 mph / 1,350 Kts / mach 2.35) -- altitude 1,400 km/h (870 mph / 756 Kts / mach 1.32) -- sea level |
| Ceiling: | 59,055 ft |
| Range: | 1,390 km (863 mi / 750 nm) -- low altitude at 497 mph 3,300 km (2,051 mi / 1,782 nm) -- high altitude at 590 mph |
| Climb Rate: | 230 m/sec (45,300 ft/min) |
| Armament | |
| One GSh-30-1 30mm cannon, plus up to 18,075 lb including R-73/R-77 AAMs, AGMs, bombs, rockets, drop tanks, and ECM pods carried on fourteen external points | |
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 Su-37 Flanker Achievements
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