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Northrop YF-23 ✕ McDonnell Douglas F-15 Eagle ✕
Manufacturer Northrop Corporation McDonnell Douglas
Description The Northrop–McDonnell Douglas YF-23 is an American single-seat, twin-engine, stealth fighter prototype technology demonstrator designed for the United States Air Force (USAF). 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 1990-08-27 1972-07-27
Entry Into service 1976-01-09
Production End 1990-01-01 1997-01-01
Designer Northrop Corporation McDonnell Douglas
Type Stealth fighter prototype Technology demonstrator
Length (m) 20.4216 19.2024
Height (m) 3.9624 5.4864
Cockpit Crew 1 1
Cruise Speed (km/h) 918.5912
Max Ceiling (m) 19800 19812
Rate of Climb (m/s) 340.614
Armament None as tested but provisions made for:; 1 × 20 mm (0.79 in) M61 Vulcan cannon; 4 × AIM-120 AMRAAM or AIM-7 Sparrow medium-range air-to-air missiles; 2 × AIM-9 Sidewinder short-range air-to-air missiles 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) 2.2 2.5
National Origin United States of America United States of America
Number Built 2 15
Powerplant Description 2 × Pratt & Whitney YF119-PW-100N or General Electric YF120-GE-100N afterburning turbofans 2 × Pratt & Whitney F100-PW-220 afterburning turbofans
Primary Users United States Air Force United States Air Force, Japan Air Self-Defense Force, Royal Saudi Air Force, Israeli Air Force
Status Canceled In service
Wikipedia Article (URL) en.wikipedia.org/wiki/Northrop_YF-23 en.wikipedia.org/wiki/McDonnell_Douglas_F-15_Eagle
Flat Wing Span (m) 13.1064 12.8016
Flat Wing Area (m²) 88.2579 56.485
Wake Category M
Aircraft Engine Pratt & Whitney F100
Number of Engines 2 2