Air Power Series>1:72 die-cast display model>F-15>HA4515
McDonnell Douglas F-15J 02-8801, ADTW, JASDF
General Background
In 1967 the U.S. became aware of the Soviet MiG-25 Foxbat. This made it necessary to develop a new aircraft to counter the MiG-25. The USAF rejected the USN F-14 Tomcat and issued its own requirements. The solution came in the form of the McDonnell-Douglas (now Boeing) F-15 Eagle. The F-15A made its inaugural flight in July 1972 and in January 1976 the first Eagle entered service. The "E" entered service in 1989. The F-15 was the first dedicated USAF air superiority fighter since the F-86 Sabre".
The Aircraft
McDonnell Douglas F-15J 02-8801 c/n 544/001 was the first of only two F-15Js actually
manufactured by McDonnell Douglas in St. Louis, Missouri. F-15J 02-8801 was delivered to the
USAF for its maiden flight on June 4, 1980 and then sent to the JASDF on July 15, 1980. A total
of two hundred and three F-15Js and twenty F-15DJs were produced for Japan. The ADTW is
the Air Development and Test Wing tasked with testing new systems and aircraft to make certain
they meet the high standards required by the JASDF.
Specifications :
Role: | C – Single-seat, all-weather, air-superiority fighter - 483 built |
D – Dual-seat variant of the C – 92 built | |
E – Dual-seat, all-weather, multi-role strike fighter - 237 built | |
Dimensions | |
Length: | C/D/E 63 ft 9 in (19.43 m) |
Wingspan: | C/D – 42 ft 10 in (13.06 m) |
E – 42 ft 9.75 in (13.05 m) | |
Height: | C/D – 18 ft 8 in (5.69 m) |
E – 63 ft 9 in (5.63 m) | |
Weight: | |
Empty: | C/D - 28,600 lb (12793 kg) |
E – 31,700 lb (14,379 kg) | |
Maximum Take-off: | C/D – 68,000 lb (30,844 kg) |
E – 81,000 lb (36,741 kg) | |
Engines: | C/D – 2 X P&W F100-PW turbofans with afterburners, each engine rated @ 25,000 thrust (11,250 kg) |
E/F – Prior to August 1991 - 2 X P&W F100-P-220 turbofans, each rated @ 14,670 ls st (65.26kN) dry and 23,830 lb st (106.0 kN) with afterburners | |
After August 1991 – 2 X P&W F100-PW-229 turbofans, each rated @ 17,800 lb st (79.18 kN) dry and 29,100 lb st (129.45 kN) with afterburners | |
Range: | |
C/D: | Ferry - 3,450 miles (3,000 nm) with CFTs + 3 X external fuel tanks |
E: | Ferry – 3,570 miles (3,100 nm) with CFTs + drop tanks |
With Drop Tanks only: | 2,765 miles (2,400 nm) |
Normal Combat Radius: | 790 miles (685 nm) |
Maximum Combat Radius: | 1,150 miles (1,000 nm) |
Speeds: | C/D – 1,875 mph (Mach 2.5 +) |
E - Maximum Level Flight Clean @ High Altitude – 1,650 mph (2,655 km/h) | |
Cruise @ Optimum Altitude – 570 mph (917 km/h) | |
Ceiling: | C/D – 65,000 ft (19,697 m) |
E – 60,000 ft (18,290 m) | |
Armament: | |
C: | 1 X M-61A1 20mm multi-barrel internal gun, 940 rounds of ammunition |
4 X AIM-9L/M Sidewinders And | |
4 X AIM-7F/M Sparrow missiles Or | |
Missile Combination - AIM-9L/M, AIM-7-F/M and AIM-120 | |
E: | 1 X M-61A1 20mm multi-barrel internal gun, 512 rounds of ammunition |
4 X AIM-9L/M Sidewinder on the under-wing stations And | |
12 X CBU-52 (6 with wing tanks) | |
12 X CBU-59 (6 with wing tanks) | |
12 X CBU-71 (6 with wing tanks) | |
12 X CBU-87 (6 with wing tanks) | |
12 X CBU-89 (6 with wing tanks) | |
20 X MK-20 (6 with wing tanks) |