Air Power Series>1:72 die-cast display model>F-4>HA1984

General Background

The F-4D was an improved “C” variant with most improvements being internal electronics and avionics. The F-4D entered operational service in April 1966 and joined the combat forces in Southeast Asia in May 1967. With the arrival of the “D” most of the “C” variant was reassigned to ground attack with the “D”s taking on the air-to-air interceptor role. In 1968 – 1969 a total of 825 “D” models were produced 793 for the USAF and 32 for the Iranian Air Force.

The Aircraft

The first of 88 German RF-4E’s that would equip AG-51 Aufklarungeschwader 51 "Immelmann" stationed at Bremgarten and AG-52 Aufklarungeschwader (Reconnaissance Wing) at Leck went into service on January 20, 1971. AG-52 was activated in December 1959 with the head of a black panther as their emblem. AG-52 became a member of the NATO Tiger Association in 1963 hosting the Meet in 1967, 1975 and 1984. RF-4E 35+76 represented AG-52 at the 1985 NATO Tiger Meet held in Kleine Brogel, Belgium. AG-52 was inactivated on December 15, 1993.

Specifications :

The RF-4E variant was an unarmed reconnaissance version for export only. Retrofitted to carry weapons by most customers.
Engines:	(2) General Electric J79-GE-17 turbojets.
Thrust:	11,870 lb. st dry, 17,900 lb. st with afterburners.
Dimensions
Length:	63 ft 0 in
Height:	16 ft 6 in
Wingspan:	38 ft 5 in
Wingarea:	530 sq ft
Performance
Cruise Speed:	585 mph
Max Speed:	1,430 mph at 36,000 ft (Mach 2.21)
	914 mph at sea level (Mach 1.19)
Landing speed:	158 mph
Initial rate of climb:	61,400 fpm
Service Ceiling:	62,250 ft
Combat Ceiling:	59,600 ft
Combat range:	595 miles
Maximum range:	1885 miles with maximum external fuel
Armament:	(1) 20-mm M61A1 cannon with 639 rounds in an under-nose gondola
	(4) AIM-7 Sparrow semi-active radar homing air-to-air missiles in semi-recessed slots in the fuselage belly.
	(2) to (4) AIM-9 Sidewinder infra-red homing air-to-air missiles carried under the wings on the inboard pylons.
	Total offensive load of up to 16,000 pounds could be carried on the centerline and four under- wing hard-points.