McDonnell Douglas
TF-4
Phantom II
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Photo: Robert Deering 6/27/2015
USS Lexington Museum (CV-16)
Corpus Christi, TexasSW

In response to Navy requirements for a high-altitude interceptor to defend carriers with long-range air-to-air missiles against attacking aircraft, McDonnell Aircraft Company delivered the F4H (later redesignated F-4) Phantom II. The aircraft's maiden flight occurred in 1958 with deliveries to Navy and Marine Corps squadrons beginning in 1960. Its performance and versatility eventually attracted the interest of not only the U.S. Air Force, but also the air forces of ten foreign nations, making it one of the most widely-employed aircraft in the history of aviation.  A small umber of F-4As were converted into two-seat training aircraft and designated TF-4. 

The Phantom II quickly demonstrated that it was a special aircraft, establishing twelve world speed, altitude, and time-to-climb records in the space of just 28 months, the pilots on some of those flights including future astronauts John Young and Richard Gordon. The escalation of the war in Vietnam thrust the F-4 into a tactical environment for which it was not originally designed, yet by war's end it had performed well in air-to-air combat and ground attack missions, with Navy and Marine Corps aviators scoring 36 kills. Under the designation RF-4, the Phantom II also served in the photo reconnaissance role.

McDonnell Douglas built 5,195 Phantom IIs during a production run that lasted from 1958 to 1979, making it second only to the MiG-21 in numbers produced. The only aircraft flown concurrently by the Navy and Air Force flight demonstration teams, the last F-4s flying in Naval Aviation retired from Marine Fighter Attack Squadron (VMFA) 112, a Reserve squadron, in January 1992, 31 years after the aircraft was first delivered to the fleet.

SPECIFICATIONS: PERFORMANCE:
Span: 38 ft., 4 7/8 in.
Length:  58 ft., 3 in
Height:  16 ft., 3 i
Empty Weight:  28,000 lb.

Gross Weight:  54,600 lb.
Crew:
Instructor and Student
Maximum speed: 1,485 mph at 48,000 ft.
Cruising speed:
Range: 2,300 miles
Service ceiling:
62,000 ft.
Engines: Two 10,900 lb. static thrust (17,000 lb. with afterburner) General Electric J-79-GE-8 turbojets
Armament: AIM-7 Sparrow and AIM-9 Sidewinder air-to-air missiles; up to 16,000 lb. of ordnance
   
SOURCE: National Museum of Naval Aviation  
VARIANTS:
 
F-4
Phantom II

RF-4
Phantom II