Air Power Series>1:72 die-cast display model>F-4>HA19048

General Background

One of the most famous and easily recognized fighter aircraft of the post-WWII era was the McDonnell F-4 Phantom II. This aircraft was developed as a private venture by the aircraft company but was soon ordered by the USN as a carrier-based attack aircraft. Its first flight took place on May 27, 1958 and it entered active service in December 1960. It wasn’t long after the F-4B appeared that a fly-off was set up with USAF front-line fighters. It was no contest, the F-4 performed so well that the USAF ordered their own variant, the F-4C. As time went on, the F-4 evolved into well over a dozen variants.

Specifications :

F4H-1 later became the F-4B
Number of “B” variant built for USN and USMC:	649
Powerplant :	2 x General Electric J79-GE-8A/-8B/-8C turbojets, 10,900 lb.s.t. dry, 17,000 lb.s.t. with afterburner
Performance
Max Speed:	@ Sea level - 845 mph
	@ 48,000 ft - 1,485 mph
Initial climb rate:	28,000 fpm
Service ceiling:	62,000 ft
Combat Ceiling:	56,850 ft
Combat range
Normal:	400 miles
Maximum range:	2,300 miles with maximum fuel load
Weights
Empty:	28,000 pounds
Gross:	44,600
Combat:	38,500 pounds
Maximum take-off:	54,600 pounds
Dimensions
Wingspan:	38 ft 5 in
Wing area:	530 sq. ft
Length:	58 ft 3.75 in
Height:	16 ft 3 in
Fuel
Maximum fuel load:
Internal in fuselage:	1,358 U.S. Gallons
Internal in wings:	630 U.S. Gallons
Total external fuel load:	1,988 U.S. Gallons
Maximum external fuel load
In center-line tank under the fuselage:	600 U.S. Gallons
In 2 x under-wing tanks:	740 U.S. Gallons
Combined fuel load:	3,328 U.S. Gallons
Armament	4 x AIM-7D or -7E Sparrow semi-active radar homing missiles in under-fuselage recesses
	Inner under-wing pylons could each accommodate an additional Sparrow or a pair of AIM-9 Sidewinder infrared homing missiles
	In ground attack mode, could carry up to 16,000 pounds of ordnance on centerline pylon underneath the fuselage and on four under-wing hard-points