HAL Tejas General characteristics
Crew: 1
Length: 13.20 m (43 ft 4 in)
Wingspan: 8.20 m (26 ft 11 in)
Height: 4.40 m (14 ft 9 in)
Wing area: 38.4 m² (413 ft²
Empty weight: 5,500 kg (12,100 lb)
Loaded weight: 8,500 kg (18,700 lb (in fighter configuration))
Max takeoff weight: 14,500 kg (32,000 lb)
Powerplant: 1× General Electric F404-GE-IN20 turbofan
Dry thrust: 54.9 kN (12,250 lbf)
Thrust with afterburner: 85 kN (19,000 lbf)
Internal fuel capacity: 3000 liters
External fuel capacity: 5×800 liter tanks or 3×1,200 liter tanks, totaling 4,000/3,600 liters
Performance
Maximum speed: Mach 1.8 (1,920+ km/h at high altitude) at 15,000 m
Range: 3000 km (1,840 mi (without refueling))
Service ceiling 15,950+ m (50,000 ft (engine re-igniter safely capable))
Wing loading: 221.4 kg/m² (45.35 lb/ft²
Thrust/weight: 1.02
g limits : +9 g / -3.5 g
JF-17-General characteristics
Crew: 1 (2 for proposed twin-seater)
Length: 14.0 m [35] (49 ft)
Wingspan: 9.45 m [35] (31 ft)
Height: 4.77 m (15 ft 8 in)
Wing area: 24.4 m² [35] (263 ft²
Empty weight: 6,450 kg [35] (14,200 lb)
Loaded weight: 9,100 kg [36] including 2× wing-tip mounted air-to-air missiles (20,062 lb)
Max takeoff weight: 12,700 kg [36] (28,000 lb)
Powerplant: 1× Klimov RD-93 turbofan [37]
Dry thrust: 49.4 kN [38] (11,106 lbf)
Thrust with afterburner: 81.4 kN [39] (18,299 lbf)
G-limit: +8.5 g [13]
Fuel Capacity: 2300kg (5,130 lb) [40]
Performance
Maximum speed: Mach 1.8 [41] [42]
Combat radius: 1,352 km [43] (840 mi)
Ferry range: 3,000km [44] [45] (1,864 mi)
Service ceiling 16,700 m [46] (54,790 ft)
Thrust/weight: 0.95 [47] [48]