Technical Specifications Su-35 (Su-27BM)

Powerplant: two 142.2 kN (31,970 lb st) NPO Saturn / UMPO AL-41F1 (izdeliye 117S) afterburning turbofans

Dimensions: length 21.9 m (71 ft 10 in) ; height 5.9 m (19 ft 4 in); wing span 15.3 m (50 ft 2½ in)

Weights: empty 18,400 kg (40,570 lb); Normal Take-Off Weight 25,300 kg (55,780 lb); Max Take-Off Weight 34,500 kg (76,060 lb); Internal Fuel: 11,500 kg (25,350 lb)

Performance: max level speed at 11,000m (36,000 ft) Mach 2.25 or 2,400 km/h (1,490 mph); at sea level 1,400 km/h (870 mph); service ceiling 18,000 m (59,000 ft); G-limit: +9

Armament: one internal GSh-301 30mm cannon with 150 rounds; up to 8,000 kg (17,640 lb) of ordnance carried on up to twelve external hardpoints, including air-to-air missiles, freefall and cluster bombs, unguided rockets, external fuel tanks, guided bombs and air-to-surface missiles.

Sources:
• Butowski, Piotr (2008). Sukhoi's Latest 'Flanker', Combat Aircraft, European Edition, Vol.9, No.3, pp. 52-55, Ian Allan Publishing Ltd, UK.
• Fomin, Andrei (2007). Su-35 - a step away from the fifth generation, Take-off, June 2007, pp. 46-53, Aeromedia Ltd, Moscow. Retrieved from www.sukhoi.org on March 27, 2008.
• Sukhoi KnAAPO (2007). Su-35 - multirole super-maneuverable fighter, sales brochure, Sukhoi Company. Retrieved from www.knaapo.ru on August 25, 2008.