General characteristics
Crew: one (pilot)
Length: 21.26 m (69 ft 9 in)
Wingspan: 12.88 m (42 ft 3 in)
Height: 4.45 m (14 ft 7 in)
Wing area: 59 m2 (630 sq ft)
Empty weight: 17,000 kg (37,479 lb)
Max takeoff weight: 36,287 kg (80,000 lb) upper estimate[2]
Powerplant: 2 × WS-10G (prototype); WS-15 when J-20 is serving afterburning turbofans dry, 180 kN (40,000 lbf) with afterburner
Maximum speed: Mach 2.0 or less (DSI limit)[82]
Range: 5,500 km (3,418 mi; 2,970 nmi)
Combat range: 2,000 km (1,243 mi; 1,080 nmi)
Service ceiling: 20,000 m (65,617 ft)
Armament
None on prototype
Production aircraft will be equipped with PL-21 LRAAM, PL-12D MRAAM, PL-10 SRAAM, LS-6 Precision Glide Bomb, 30mm cannon, up to four rocket launchers, two IR decoy launchers, air-to-surface missiles and smart bombs.
No comments:
Post a Comment