Hobby Master Archive

True 1/72 scale. Professionally painted. Great attention to detail. All markings are Tampoed (pad applied). Option to display the model on a stand that is provided. Model can be shown with the landing gear in the down or up positions. Canopy can be displayed open or closed. Pilot figures included. Extremely heavy metal with a minimum of plastic. Highly collectable.

Hobby Master 1/72 Air Power Series HA1984 McDonnell Douglas RF-4E Phantom II AG 52, NATO Tiger Meet, Kleine Brogel, Belgium,1985

The McDonnell Douglas F-4 was the main multipurpose aircraft for the US Military for 20 years. The F-4E variant was an improved version of the C/D with an elongated nose and compact radar. These two things made it possible to install a 20mm M61A1 6 barrel 640 round Vulcan gun pod in the nose. The F-4E was the most produced variant with 1387 aircraft being made over its 12 year production period. The “E” also equipped more air forces than any other variant of the Phantom II.

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 McDonnell Douglas F-4E Phantom II Note - 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.

Fuel Maximum internal fuel - fuselage tanks 1,364 US gallons (up to block 40) and 1,225 US gallons (from block 41 on). Additional - 630 gallons of fuel in internal wing tanks. External fuel load - 600 US gallons centerline tank. Additional - 370 US gallons tanks under each wing attached to the outer pylon. Total fuel load - 3334 US gallons (up to block 40) or 3195 US gallons (from block 41 on).

Performance Maximum speed - 1,430 mph at 36,000 ft (Mach 2.21) 914 mph at sea level (Mach 1.19) Cruising speed - 585 mph Landing speed - 158 mph Initial climb rate - 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

Weights Empty - 29,535 lbs Gross - 40,562 lbs Combat - 38,019 lbs Take off - 61,651 lbs Dimensions Wingspan - 38 ft 5 in Wing area - 530 sq ft Length - 63 ft 0 in Height - 16 ft 6 in

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.