McDonnell Douglas F-15E Strike Eagle
| GENERAL DATA | |||
| Type |
Multirole strike fighter
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| Manufacturer(s) | McDonnell Douglas Boeing Defense, Space & Security |
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| Prototype first flight | 11 December 1986 |
Introduction | 30 September 1989 |
| Produced | 1985–present |
Number built | F-15E : 236 F-15I : 25 F-15K : 61 F-15S : 72 |
| Status | In service |
Crew | 2 (Pilot and weapon systems officer) |
| DIMENSIONS | |||
| Length | 19.43 m |
Empty Weight | 14300 kg |
| Wingspan | 13.05 m |
Loaded Weight | ? kg |
| Height | 5.63 m |
Max takeoff weight | 36700 kg |
| Wing area | 56.5 m² |
Wing loading | 301.3 kg/m² |
| ARMAMENT | ||||
| Guns | 1× 20 mm (0.787 in) M61A1
Vulcan nose mounted 6-barrel rotary cannon |
Ammunition Carried |
500 |
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| Hardpoints | 2 wing pylons, fuselage pylons,
bomb racks on CFTs with a capacity of 10400 kg of external fuel
and ordnance
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| Missiles | Air-to-air missiles | 4× AIM-9 Sidewinder 8× AIM-120 AMRAAM |
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| Air-to-surface missiles | 6× AGM-65 Maverick 2× AGM-84 Harpoon 2× AGM-84H/K SLAM-ER AGM-130 AGM-154 JSOW AGM-158 JASSM |
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| Bombs | Mark 82 bomb Mark 84 bomb Mark 77 bomb incendiary GBU-15 GBU-10 Paveway II GBU-12 Paveway II GBU-24 Paveway III GBU-27 Paveway III GBU-28 (Bunker buster) GBU-31 or GBU-38 {8 GBU-31s or 16 GBU-38s} (JDAM) GBU-54 Laser JDAM (LJDAM) GBU-39 Small Diameter Bomb (SDB) B61 or B83 nuclear bomb CBU-87 or CBU-103 (CEM) CBU-89 or CBU-104 (GATOR) CBU-97 or CBU-105 (SFW) CBU-107 Passive Attack Weapon BLU-107 Durandal |
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| POWERPLANT | |||
| Engine | 2 ×
Pratt & Whitney F100-PW-220 or -229 afterburning turbofans
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| Dry thrust | (64.9 kN
for -220) each |
Thrust with afterburner | (105.7 kN for -220) each or 13 154 kgp (129.7 kN for -229) each |
| Thrust/weight | 0.93
|
Fuel Capacity | 5952 kg internally* |
(*) up to 3× 2300 L external drop
tanks for ferry flight or extended range/loitering time
1x 1800 litres Super cruise drop tank.
| PERFORMANCES | |||
| Maximum Speed | 2665+
km/h (Mach 2.5+) at high altitude 1450 km/h (Mach 1.2) at low altitude |
Cruise Speed | 917 km/h |
| Rate of Climb | 254+ m/s |
Service ceiling | 18200 m |
| Combat Range | 1270 km |
Ferry Range | 3900 km with conformal fuel tank and three external fuel tanks |
| Sources | |||
| Wikipédia | aviationsmilitaires.net | ||
Drawings |
