ARMSNET
Military Equipment Database
Initializing 0%

F-2

F-2

Multi-Role Fighters
Spotted an error? Sign in to suggest an edit.
Basic Information
Name
F-2
Designation
F-2
Alternate Designation
F-2A (single-seat), F-2B (twin-seat), XF-2
Equipment Type
Multi-Role Fighters
Manufacturer
Lockheed Martin, Mitsubishi Heavy Industries
Date of Introduction
2002
Description

The Japanese Air Self-Defense Force (JASDF) F-2, XF-2 prototype, is a derivative of the combat-proven F-16C/D Fighting Falcon being developed between the United States/Lockheed-Martin (40 percent) and Japan/Mitsubishi Heavy Industries (60 percent). The F-2 multi-role fighter is superseding the F-1 aircraft in the Japanese Self-Defense Forces. The F-2 features advanced active phased array radar (J/APG-1), waves absorbing materials, an enlarged wing area over the F-16 (25 percent approximately) providing greater fuel load, a more powerful engine, two additional weapon stations over the F-16, and enlarged fuselage and horizontal tails. The majority of avionics and electronic equipment are produced in Japan. Despite the F-2 is air-to-air and air-to-surface capable, the aircraft will be used for the air-to-surface role specially for anti-ship missions employing ASM-2 missiles. The Japanese government has authorized production of 94 F-2s with the goal of procuring up to 130 aircraft. In 2011 the Japanese government decided to add the JDAM guided bomb capability to the F-2A/B aircraft fleet. The J/APG-2 upgraded radar will be provided to the fleet of F-2 jets beginning in 2015.

Air & Air Defense Specifications
Crew 1
Max Speed 2716.6 km/h
Range 2000.0 km
Service Ceiling 20000 m
Wingspan 11.10 m
Overview (Deagel)
Group Multi-Role Fighters
Status Active
Also Known As F-2A (single-seat), F-2B (twin-seat), XF-2
Origin Japan, United States of America
Contractors Lockheed Martin, Mitsubishi Heavy Industries
Initial Operational Capability (IOC) 2002
Total Production 130
Specifications (Deagel)
Crew 1
Number of Engines 1
Dimensions — Height 5 meter
Dimensions — Length 15.5 meter
Dimensions — Main Gun Caliber 20 millimeter
Dimensions — Wingspan 11.1 meter
Mass — Max Takeoff Thrust 29,000 pound
Mass — Max Takeoff Weight 22,000 kilogram
Performance — Ceiling 20,000 meter
Performance — Max Range 2,000 kilometer
Speed — Top Speed at High Altitude 2.2 mach
Gear (Deagel)
Item 1 Air-to-Air Missiles: AAM-3 (2)
Item 2 Air-to-Air Missiles: AAM-4 (4)
Item 3 Air-to-Air Missiles: AAM-4B (4)
Item 4 Anti-Ship Missiles: ASM-2 (4)
Item 5 Anti-Ship Missiles: XASM-3 (2)
Item 6 Bombs: GBU-30 JDAM (4)
Item 7 Bombs: GBU-31 JDAM (4)
Item 8 Bombs: GBU-32 JDAM (4)
Item 9 Bombs: GBU-35 JDAM (4)
Item 10 Bombs: GBU-38 JDAM (4)
Item 11 Fighter Aircraft Engines: F110-GE-129 (1)
Item 12 Medium Caliber Cannons: M61A1 (1)
Item 13 Optronic Systems: PANTERA (1)
Item 14 Radar Systems: J/APG-1 (1)
Item 15 Radar Systems: J/APG-2 (1)
Details
Country of Origin Japan
Category Multirole Aircraft
Air > Multirole Aircraft
Classification
Domain
Air & Air Defense
Equipment Status
Active
Dimensions
Length
15.5 m
Width
11.1 m
Height
5 m
Weight
22000 kg
Related Equipment (1)
Operators (1)
Japan
Something went wrong. Please reload the page. Reload