Hauptkampfflugzeug J-23 Specs Crew: 1 Length: 20.1 m (65 ft 11 in) Wingspan: 14.1 m (46 ft 3 in) Height: 4.6 m (15 ft 1 in) Wing area: 78.8 m2 (848 sq ft) Empty weight: 18,000 kg (39,683 lb) Gross weight: 25,000 kg (55,116 lb) normal takeoff weight, 29,270 kg (64,530 lb) at full load Max takeoff weight: 35,000 kg (77,162 lb) Fuel capacity: 10,300 kg (22,700 lb) Powerplant: 2 × Saturn AL-41F1 afterburning turbofan, 88.3 kN (19,900 lbf) thrust each dry, 142.2 kN (32,000 lbf) with afterburner, 147.1 kN (33,100 lbf) in emergency power Performance Maximum speed: Mach 2 (2,135 km/h; 1,327 mph) at altitude Mach 1.3 (1,400 km/h; 870 mph) supercruise at altitude Range: 3,500 km (2,200 mi, 1,900 nmi) subsonic, 4,500 km from 2 outboard fuel tanks[250] Supersonic range: 1,500 km (930 mi, 810 nmi) Service ceiling: 20,000 m (66,000 ft) g limits: +9.0 Wing loading: 371 kg/m2 (76 lb/sq ft) normal takeoff weight Thrust/weight: 1.16 at normal takeoff weight (0.99 at loaded weight with full fuel)
Inspired by Su-57
