F-2 ติดอาวุธได้ทุกอย่างที่ F16 ติดตั้งได้ครับ เพิ่มเติมตรงที่ติดอาวุของญี่ปุ่นเองได้ด้วย
Mitsubishi F-2
Role Multirole fighter
National origin Japan, United States
Manufacturer Mitsubishi , Lockheed Martin
First flight 7 October 1995
Introduced 2000
Primary user Japan Air Self-Defense Force
Number built 94
Unit cost US$108 million in 2004
Developed from F-16 Fighting Falcon
a 25% larger wing area
composite materials used to reduce overall weight and radar signature
longer and wider nose to accommodate a phased-array radar
larger tailplane
larger air intake
three-piece cockpit canopy
capabilities for four ASM-1 or ASM-2 anti-ship missiles, four AAMs, and additional fuel tanks
Specifications (F-2A)
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: 15,000 kg (33,000 lb)
Max takeoff weight: 22,100 kg (48,700 lb)
Powerplant: 1× General Electric F110-GE-129 turbofan, 76 kN military thrust, 131 kN with afterburner
(17,000 lbf military thrust 29,500 lbf with afterburner)
Performance
Maximum speed: Mach 2.0 at altitude
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 8085 kg:
AAMs: AIM-9 Sidewinder, AIM-7 Sparrow, Mitsubishi AAM-3, Mitsubishi AAM-4
air-to-ground weapons include: ASM-1 and ASM-2 anti-ship missiles, various free-fall bombs with GCS-1 IIR seeker heads
Avionics
Mitsubishi Active Electronically Scanned Array radar system.
