Sukhoi T-50 PAK FA (ПАК ФА)(Prospective Airborne Complex of Frontline Aviation) Specs:- General characteristics Crew: 1 Length: 19.8 m (65.0 ft) Wingspan: 13.95 m (45.8 ft) Height: 4.74 m (15.6 ft) Wing area: 78.8 m2 (848.1 ft2) Empty weight: 18,000 kg (39,680 lb) Loaded weight: 25,000 kg (55,115 lb) typical mission weight, 28,300 kg (62,390 lb) at full fuel Max. takeoff weight: 35,000 kg (77,160 lb) Powerplant: 2 × NPO Saturn izdeliye 117 (AL-41F1) for initial production, izdeliye 30 for later production[83] thrust vectoring turbofan Dry thrust: 2 x 24,300 lbf Thrust with afterburner: 2 x 39,600 lbf Fuel capacity: 10,300 kg Performance Maximum speed: At altitude: Mach 2.3 (2,440 km/h, 1,520 mph) Supercruise: Mach 1.6 (1,700 km/h, 1,060 mph) Range: 3,500 km (2,175 mi) subsonic Ferry range: 5,500 km (3,420 mi) with one in-flight refueling Service ceiling: 20,000 m (65,000 ft) Wing loading: 317–444 kg/m2 (65–91 lb/ft2) Thrust/weight: Saturn 117: 1.06 (1.19 at typical mission weight) izdeliye 30: 1.24 (1.41 at typical mission weight) Maximum g-load: +9.0 g Armament Guns: Provision for 1× 30 mm GSh-301 cannon in right LEVCON root Air to air loadout: 6× K-77M or 4× izdeliye 810 2× K-74M2 or 2× izdeliye 300 Air to ground loadout: 4× Kh-38M or 4× Kh-58UShK or 8× KAB-250 or 4× KAB-500 2× K-74M2 or 2× izdeliye 300 Air to sea loadout: 4× Kh-35 2× K-74M2 or 2× izdeliye 300 Hardpoints: Six external hardpoints. Kh-31 R-73 R-77 Avionics Sh121 multifunctional integrated radio electronic system (MIRES) N036 Byelka radar system N036-1-01: Frontal X-band AESA radar N036B-1-01: Cheek X-band AESA radars for increased angular coverage N036L-1-01: Slat L-band arrays for IFF L402 Himalayas ECM suite 101KS Atoll electro-optical system 101KS-O: Laser directional infrared countermeasures 101KS-V: Infrared search-and-track 101KS-U: Ultraviolet missile approach warning system 101KS-N: Targeting pod
Posted on: Sat, 03 Jan 2015 16:36:52 +0000