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McDonnell Douglas F-15 STOL/MTD ✕ McDonnell Douglas F-15 Eagle ✕
Manufacturer McDonnell Douglas McDonnell Douglas
Description The McDonnell Douglas F-15 STOL/MTD (Short Takeoff and Landing/Maneuver Technology Demonstrator) is a modified F-15 Eagle. 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 1988-09-07 1972-07-27
Entry Into service 1976-01-09
Production End 1997-01-01
Service End 1991-08-15
Designer McDonnell Douglas McDonnell Douglas
Type Technology Demonstrator and Research Aircraft
Length (m) 19.42 19.2024
Height (m) 5.64 5.4864
Cockpit Crew 2 1
Max Speed (km/h) 2124.334
Cruise Speed (km/h) 918.5912
Max Ceiling (m) 18288 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)
Capacity Description 17,000 lb (7,112 kg)
Max Mach (Mach) 2 2.5
National Origin United States of America United States of America
Number Built 1 15
Powerplant Description 2 × Pratt & Whitney F100-PW-229 turbofan engines, equipped with 20° three-dimensional thrust vectoring P/YBBN, 79 kN thrust each 2 × Pratt & Whitney F100-PW-220 afterburning turbofans
Primary Users United States Air Force, NASA United States Air Force, Japan Air Self-Defense Force, Royal Saudi Air Force, Israeli Air Force
Status Retired from both NASA and military service In service
Wikipedia Article (URL) en.wikipedia.org/wiki/McDonnell_Douglas_F-15_STOL/MTD en.wikipedia.org/wiki/McDonnell_Douglas_F-15_Eagle
Flat Wing Span (m) 13 12.8016
Flat Wing Area (m²) 56.5 56.485
Wake Category M
Aircraft Engine Pratt & Whitney F100 Pratt & Whitney F100
Number of Engines 2 2