
Hobby Master 1/72 Air Power Series (Jet Powered) HA1910 - McDonnell-Douglas F- 4E Phantom II USAF Air Demonstration Team "Thunderbird 1" 1970's |

| Specifications for the standard production McDonnell Douglas F-4E Phantom II Engines - 2 X 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 X 20-mm M61A1 cannon with 639 rounds in an under-nose gondola 4 X AIM-7 Sparrow semi-active radar homing air-to-air missiles in semi-recessed slots in the fuselage belly 2 to 4 X 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. The Thunderbird's aircraft were stripped of all weapons and any unnecessary equipment. |