Mitsubishi T-2 - Specifications (T-2(K))

Specifications (T-2(K))

Data from Jane's All The World's Aircraft 1976-77

General characteristics

  • Crew: Two
  • Length: 17.85 m (58 ft 6¾ in)
  • Wingspan: 7.88 m (25 ft 10¼ in)
  • Height: 4.39 m (14 ft 4¾ in)
  • Wing area: 21.2 m² (228 ft²)
  • Airfoil: NACA 65 series (modified)
  • Empty weight: 6,197 kg (13,662 lb)
  • Loaded weight: 9,675 kg (21,330 lb)
  • Max. takeoff weight: 12,800 kg (28,219 lb)
  • Powerplant: 2 × Ishikawa-Harima TF40-801A afterburning turbofans
    • Dry thrust: 20.95 kN (4,710 lbf) each
    • Thrust with afterburner: 31.76 kN (7,140 lbf) each

Performance

  • Maximum speed: 1,700 km/h (1,056 mph, 917 kn) at 10,975 m (36,000 ft) (clean)
  • Ferry range: 2,870 km (1,785 mi, 1,550 nmi)
  • Service ceiling: 15,240 m (50,000 ft)

Armament

  • Guns: 1 × 20 mm JM61A1 cannon
  • Hardpoints: One centreline and two underwing pylons
  • Missiles: Provision for Two AIM-9 Sidewinder Air-to-air missile on wingtip missile rails

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