| McDonnell Douglas F-4 Phantom II ✕ | |
|---|---|
| Manufacturer | McDonnell Aircraft |
| Description | The McDonnell Douglas F-4 Phantom II is an American tandem two-seat, twin-engined, all-weather, long-range supersonic jet interceptor and fighter-bomber that was developed by McDonnell Aircraft for the United States Navy. |
| First Flight | 1958-05-27 |
| Entry Into service | 1960-12-30 |
| Production End | 1981-01-01 |
| Designer | McDonnell Aircraft |
| Length (m) | 19.2 |
| Height (m) | 5 |
| Cockpit Crew | 2 |
| Max Speed (km/h) | 2370 |
| Cruise Speed (km/h) | 940 |
| Max Ceiling (m) | 18288 |
| Rate of Climb (m/s) | 209.804 |
| Armament | E-model has a 20 mm (0.787 in) M61A1 Vulcan cannon mounted internally under the nose, 640 rounds; Up to 18,650 lb (8,480 kg) of weapons on nine external hardpoints, including general-purpose bombs, cluster bombs, TV- and laser-guided bombs, rocket pods, air-to-ground missiles, anti-ship missiles, gun pods, and nuclear weapons. Reconnaissance, targeting, electronic countermeasures, baggage pods, a… |
| Max Mach (Mach) | 2.23 |
| National Origin | United States of America |
| Number Built | 5195 |
| Powerplant Description | 2 × General Electric J79-GE-17A after-burning turbojet engines |
| Primary Users | United States Air Force (historical) |
| Status | In limited service |
| Wikipedia Article (URL) | en.wikipedia.org/wiki/McDonnell_Douglas_F-4_Phantom_II |
| Flat Wing Span (m) | 11.7 |
| Flat Wing Area (m²) | 49.2 |
| Flat Wing Aspect Ratio | 2.77 |
| Number of Engines | 2 |