Specifications (J-22M)
Three point viewData from Jane's All The World's Aircraft 1993-94[3]
General characteristics
Crew: one or two,pilot
Length: 13.02 m (42 ft 8½ in)
Wingspan: 9.30 m (30 ft 6¼ in)
Height: 4.52 m (14 ft 10 in)
Wing area: 26.00 m² (279.9 ft²)
Empty weight: 5,550 kg (12,125 lb)
Max takeoff weight: 11,080 kg (24,427 lb)
Powerplant: 2 × Turbomecanica/Orao-built Rolls-Royce Viper Mk 633-47 turbojet
Dry thrust: 17.79 kN (4,000 lbf) each
Thrust with afterburner: 22.24 kN (5,000 lbf) each
Performance
Maximum speed: 1,130 km/h (610 knots, 702 mph) at sea level
Stall speed: 185 km/h (100 knots, 115 mph)
Combat radius: 522 km (282 nmi, 324 mi) (four BL755 cluster bombs and one 1,500 L drop tank)
Ferry range: 1,320 km ()
Service ceiling: 15,000 m (49,210 ft)
Rate of climb: 89 m/s (17,520 ft/min)
Armament
Guns: 2 × 23 mm GSh-23L cannons
Hardpoints: Five (four underwing and one centreline) with a capacity of 500 kg (1,100 lb) (wing pylons), 800 kg (1,770 lb) (centreline pylons) - total capacity 2,800 kg (6,200 lb)
Missiles: AGM-65 Maverick TV guided AGM or Grom-1 Radio-guided AGM (based on Soviet Kh-23)
Bombs: MK series bombs, BL755 cluster bombs, Durandal runway attack bombs
