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Advanced derivative of the Su-27 "Flanker".
The first Su-27M prototype flew in 1985 and was
displayed at the 1992 Farnborough Air Show.
Changes from the Su-27 include a new radar,
foreplanes, more powerful
engines, an enlarged and improved infrared search and track unit in front
of the cockpit, an infrared missile-warning
scanner on the fuselage spine and a large "spine" between the engines
containing a rearward-facing air-to-air radar, allowing the use of
rear-firing missiles mounted on rotating pylons
that can fire missiles in either direction. Not present on the prototype,
but expected to be on the production version, are two-dimensional
thrust-vectoring engine nozzles.
 | A three-view drawing (1000 x 498) |
| MODEL | Su-35 |
| CREW | 1 |
| ENGINE | 2 x Lyulka AL-35F turbofans, 145.0kN |
| WEIGHTS |
| Take-off weight | 36000 kg | 79367 lb |
| Empty weight | 18400 kg | 40565 lb |
| DIMENSIONS |
| Wingspan | 14.70 m | 48 ft 3 in |
| Length | 21.96 m | 72 ft 1 in |
| PERFORMANCE |
| Max. speed | 2440 km/h | 1516 mph |
| Ceiling | 18000 m | 59050 ft |
| Range w/max.fuel | 3500 km | 2175 miles |
| ARMAMENT | 1 x 30mm cannon, 8000kg of weapons on 14 external hardpoints |
| Sykhoi, 08.09.2008 gg)) +1! | | ÇÑÀºÈ£, ggamcool(@)nate.com, 18.05.2008 dd |
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