General Specifications
Contractor : McDonnell Douglas Aerospace
Nation of origin : USA
Function: Air superiority and attack
Crew : F-15A/C-1, F-15B/D/E-2
Date of introduction : 1968
In-service year : F-15A/B – 1973, F-15C/D – 1979, F-15E
- 1988
Dimensions
Wing span : 13.05m / 42 ft 10 in
Length : 19.43m / 63 ft 9 in
Height : 5.63m / 18 ft 6 in
Weight :
F-15C
: 44,630 lb empty / 68,000 lb max. take off
F-15E
: 32,000 lb empty / 81,000 lb max. take off
Ceiling : 60,000 ft
Speed : 2,655 km/h / 1,650 mph
Range : 5,725 km / 3,570 miles with FAST packs
Engine :
F15C : Two Pratt &
Whitney F100-P-200 afterburning turbofan, 23,770 lb thrust each
F15E : Two Pratt &
Whitney F100-Pw-229 afterburning turbofan, 29,100 lb thrust each
Armament:
F15C - One M61A1 Vulcan 20mm six-barrel cannon with
940 rounds,plus up to 23,600 lb including nuclear weapons, ASMs, bombs,
rockets, dispenser weapons, drop tanks and ECM pods carried on nine external
points.
F15E - One M61A1 Vulcan 20mm six-barrel cannon with
512 rounds,plus up to 24,250 lb including nuclear weapons, cluster bombs,
laser-guided bombs, AGM-65 Maverick ASMs, AGM-88 HARMs, AIM-7 Sparrow AAMs,
AIM-120 AMRAAMs, and three fuel tanks on up to eighteen external points.
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