McDonnell Douglas F-15 Eagle
Cruise Speed
918.5912 km/h
Entry Into service
1976-01-09
Maximum Take-Off Weight
30.8443 t (paragliders: kg)
Maximum Range
3970.688 km
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All data (27 fields)
- Name
- McDonnell Douglas F-15 Eagle
- Manufacturer
- McDonnell Douglas
- Description
- The McDonnell Douglas F-15 Eagle is an American twin-engine, all-weather fighter aircraft designed by McDonnell Douglas (now part of Boeing).
- ICAO Code
- F15
- First Flight
- 1972-07-27
- Entry Into service
- 1976-01-09
- Production End
- 1997-01-01
- Designer
- McDonnell Douglas
- Length (m)
- 19.2024
- Height (m)
- 5.4864
- Cockpit Crew
- 1
- Cruise Speed (km/h)
- 918.5912
- Max Ceiling (m)
- 19812
- Rate of Climb (m/s)
- 340.614
- Armament
- 1× 20 mm (0.787 in) M61A1 Vulcan 6-barrel rotary cannon, 940 rounds; Total 9: two under-wing (each with additional two missile launch rails), four under-fuselage (for semi-recessed carriage of AIM-7 or AIM-120) and a single centerline pylon station, optional fuselage pylons (which may include conformal fuel tanks)
- Max Mach (Mach)
- 2.5
- National Origin
- United States of America
- Number Built
- 15
- Powerplant Description
- 2 × Pratt & Whitney F100-PW-220 afterburning turbofans
- Primary Users
- United States Air Force, Japan Air Self-Defense Force, Royal Saudi Air Force, Israeli Air Force
- Status
- In service
- Wikipedia Article (URL)
- en.wikipedia.org/wiki/McDonnell_Douglas_F-15_Eagle
- Flat Wing Span (m)
- 12.8016
- Flat Wing Area (m²)
- 56.485
- Wake Category
- M
- Aircraft Engine
- Pratt & Whitney F100
- Number of Engines
- 2