Specifications (F-2A)
Data from Wilson
General characteristics
- Crew: 1 (or 2 for the F-2B)
- Length: 15.52 m (50 ft 11 in)
- Wingspan: 11.13 m (36 ft 6 in)
- Height: 4.69 m (15 ft 5 in)
- Wing area: 34.84 m² (375 ft²)
- Empty weight: 9,527 kg (21,000 lb)
- Loaded weight: 14,970 kg (33,000 lb)
- Max. takeoff weight: 18,100 kg (48,700 lb)
- Powerplant: 1 × General Electric F110-GE-129 turbofan
- Dry thrust: 76 kN (17,000 lbf)
- Thrust with afterburner: 120–125 kN (29,500 lbf)
Performance
- Maximum speed: Mach 2.0 (2 469.6 km/h, 1 333 kn)
- Range: 834 km on anti-ship mission (520 miles)
- Service ceiling: 18,000 m (59,000 ft)
- Wing loading: 430 kg/m² at weight of 15,000 kg (88 lb/ft²)
- Thrust/weight: 0.89
Armament
- 20 mm JM61A1 cannon, plus maximum weapon load of 8,085 kg:
- AAMs: AIM-9 Sidewinder, AIM-7 Sparrow, Mitsubishi AAM-3, Mitsubishi AAM-4 (from FY2010)
- air-to-ground weapons include: ASM-1 and ASM-2 anti-ship missiles, various free-fall bombs with GCS-1 IIR seeker heads, JDAM
- others: J/AAQ-2 FLIR
Avionics
- Mitsubishi Active Electronically Scanned Array radar system including J/APG-1
Read more about this topic: Mitsubishi F-2