Length: 17"
Wingspan: 11"
Scale: 1/45
Missiles and bombs attached. Includes desk stand.
The McDonnell Douglas F-4 Phantom II is a tandem two-seat, twin-engined, all-weather, long-range supersonic jet interceptor fighter/fighter-bomber originally developed for the U.S. Navy by McDonnell Aircraft. Proving highly adaptable, it became a major part of the air wings of the United States Navy, Marine Corps, and Air Force. It was used extensively by all three of these services during the Vietnam War, serving as the principal air superiority fighter for both the Navy and Air Force, as well as being important in the ground-attack and reconnaissance roles by the close of U.S. involvement in the war.
First entering service in 1960, the Phantom continued to form a major part of U.S. military air power throughout the 1970s and 1980s, being gradually replaced by more modern aircraft such as the F-15 Eagle and F-16 Fighting Falcon in the U.S. Air Force; the F-14 Tomcat and F/A-18 Hornet in the U.S. Navy; and the F/A-18 in the U.S. Marine Corps. It remained in use by the U.S. in the reconnaissance and Wild Weasel roles in the 1991 Gulf War, finally leaving service in 1996. The Phantom was also operated by the armed forces of 11 other nations. Israeli Phantoms saw extensive combat in several ArabÐIsraeli conflicts, while Iran used its large fleet of Phantoms in the IranÐIraq War. Phantoms remain in front line service with seven countries, and in use as an unmanned target in the U.S. Air Force.
Phantom production ran from 1958 to 1981, with a total of 5,195 built. This extensive run makes it the second most-produced Western jet fighter, behind the F-86 Sabre at just under 10,000 examples.
F-4J
Improved F-4B version for US Navy and Marines, with emphasis on air-to-air combat capability improvement, which include: J79-GE-10 engines with 17,844 lbf (79.374 kN) of afterburner thrust each, AN/APG-59 pulse doppler radar coupled with the AN/AWG-10 Fire Control System for look-down shoot-down capability, larger main landing gear wheels resulting in wing bulges similar to F-4C, slatted tailplane, alierons drooped 16.5¡ when landing gear and flaps were deployed to decrease the landing speed, zero-zero ejection seats, expanded ground attack capability, no IRST sensor under the nose; 522 built.
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