| Manufacturer |
McDonnell Aircraft |
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. |
The McDonnell F-101 Voodoo is a supersonic jet fighter designed and produced by the American McDonnell Aircraft Corporation. |
| First Flight |
1958-05-27 |
1954-09-29 |
| Entry Into service |
1960-12-30 |
1957-05-01 |
| Production End |
1981-01-01 |
|
| Service End |
|
1972-01-01 |
| Designer |
McDonnell Aircraft |
McDonnell Aircraft |
| Type |
|
Fighter aircraft |
| Length (m) |
19.2 |
20.4216 |
| Height (m) |
5 |
5.4864 |
| Cockpit Crew |
2 |
2 |
| Max Speed (km/h) |
2370 |
1824.996 |
| Cruise Speed (km/h) |
940 |
|
| Max Ceiling (m) |
18288 |
17800.32 |
| 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… |
4 (originally 6) × AIM-4 Falcon or 2 × AIR-2 Genie nuclear rockets, plus 2 × AIM-4 Falcon |
| Max Mach (Mach) |
2.23 |
1.72 |
| National Origin |
United States of America |
Macao |
| Number Built |
5195 |
807 |
| Powerplant Description |
2 × General Electric J79-GE-17A after-burning turbojet engines |
2 × Pratt & Whitney J57-P-55 afterburning turbojet engines |
| Primary Users |
United States Air Force (historical) |
United States Air Force (historical), Republic of China Air Force (historical), Royal Canadian Air Force (historical) |
| Status |
In limited service |
Retired |
| Wikipedia Article (URL) |
en.wikipedia.org/wiki/McDonnell_Douglas_F-4_Phantom_II |
en.wikipedia.org/wiki/McDonnell_F-101_Voodoo |
| Flat Wing Span (m) |
11.7 |
11.8872 |
| Flat Wing Area (m²) |
49.2 |
34.1883 |
| Flat Wing Aspect Ratio |
2.77 |
|
| Number of Engines |
2 |
2 |