McDonnell F-4 Phantom II
Summary
Category | Combat aircraft |
Origin country | 🇺🇸 United States |
First flight | 27 May 1958 |
Year of introduction | 1962 |
Number produced | 5195 units |
Average unit price | $3 million |
Description
The F-4 Phantom II was a large twin-engine aircraft designed for all-weather air superiority and attack missions. Named Phantom II in honor of the FH-1 Phantom, a fighter aircraft built in the 1940s by the same company, the F-4 was the first American multi-role fighter. Initially used as an interceptor by the US Navy, it was later adopted by the US Marine Corps for ground support and attack missions. The Phantom II set numerous altitude and speed records in the early 1960s. It saw extensive service during the Vietnam War and was capable of operating from aircraft carriers.
The early versions of the F-4 were initially built without the traditional cannon, but it was quickly realized that this weapon was essential for air combat. The first generations were therefore equipped with external pods, and starting from the E variant, it was fitted with an internal 20mm cannon. Though effective and robust, this heavy aircraft suffered from a lack of maneuverability. The navigator, seated behind the pilot, could take control in case of emergencies. A specialized version for Wild Weasel missions, which involved destroying anti-aircraft defenses, called the F-4G, was developed later on.
Production of the F-4 Phantom II ended in 1979, with a total of 5,057 units built across 15 different versions. The last F-4s were retired from US military service in 1996, but this aircraft is still in use in some countries.
Technical specifications
Version: F-4E | |
---|---|
Crew | 1 pilot + 1 WSO |
Operational range | 680 km (423 mi) |
Maximum speed | 2370 km/h (1473 mph) |
Wing area | 49.2 m² (529.6 sqft) |
Wingspan | 11.7 m (38.4 ft) |
Height | 5 m (16.4 ft) |
Length | 19 m (62.3 ft) |
Service ceiling | 18288 m (60000 ft) |
Empty weight | 13757 kg (30329 lbs) |
Max. takeoff weight | 28030 kg (61795 lbs) |
Climb rate | 210.0 m/s (689.0 ft/s) |
Takeoff distance | 1370 m (4495 ft) |
Powerplant | 2 × turbojets General Electric J79-GE-17A delivering 8093 kgp |
Ejection seat | Martin-Baker Mk 7 |
Current operating countries
Country | Units | ||
---|---|---|---|
South Korea | 69 | ||
Iran | 63 | ||
Turkey | 48 | ||
Greece | 33 |
Numbers in parentheses, e.g. '(+5)', indicate units ordered but not yet delivered.
All operators
Australia • Germany • Egypt • Spain • United Kingdom • Greece • Iran • Israel • Japan • South Korea • Turkey • United States
Armament
Missiles payload:
- Anti-Radiation AGM-45 Shrike
- Air-to-Surface AGM-65 Maverick
- Anti-Radiation AGM-78 Standard ARM
- Anti-Radiation AGM-88 HARM
- Air-to-Air Medium-Range AIM-7 Sparrow
- Air-to-Air Short-Range Raytheon AIM-9 Sidewinder
Bombs payload:
- Cluster Aerojet CBU-87/B CEM
- Cluster CBU-58
- Cluster CBU-89/B Gator
- Low-Drag Mk 82
- Low-Drag Mk 84
- Laser-Guided Raytheon GBU-10 Paveway II
- Laser-Guided Raytheon GBU-12
- Guided Rockwell GBU-15(V)1/B MGWS