Sukhoi Su-34 Platypus Su-34 Wing: span 14.70 m (48 ft 2.75 in); aspect ratio 5.6; wing area 46.50 m2 (500.54 sq ft) Fuselage and tail: length 21.90 m (71 ft 10 in) height 5.90 m (19 ft 4 in~; tailplane span 9.90 m (32 ft 6 in); wheel track 4.33 m (14 ft 2.5 in); wheel base 5.88 m (19 ft 3.5 in) Powerplant: Two NPO Saturn/Lyul'ka, AL-31 FM turbofans, each rated at 130.42 kN (29,320 lb st) with afterburning) Weights: empty 17700 kg (39,021 lb); normal take-off 23250 kg (51,257 lb); maximum take off 44,360 kg (97,795 lb) Fuel and load: normal internal fuel load about 5270 kg (11,618 lb);maximum internal fuel 9400 kg (20,723 lb); maximum ordnance 8,000 kg (17,636 lb) Speed: limiting Mach 2.35; maximum level speed at 11000 m (36,000 ft) Mach 1.8 and at sea level Mach 1.15 1,400 km/h, 870 mph) Range: with maximum internal fuel 4,000 km (2,160 km: 2,485 miles~ Performance: maximum rate of climb at sea level 19800 m (64,960 ft) per minute: service ceiling 17,000 m (55,755 ft): take-off run 450 m (1,476 ft) at maximum take-off weight; landing run 700 m (2,297 ft) at normal landing weight g limits: + 8
PROGRAMME: DESIGN FEATURES: POWER PLANT: ACCOMMODATION: Two crew side by side on K-36 zero/zero ejection seats. Access to cockpit via door in nosewheel bay; area protected with 17 mm (2/3 in) thick titanium; toilet and galley installed. AVIONICS: ARMAMENT: |
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