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F-4 Phantom II vs. MiG-23

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F-4

vs.

MiG-23

Role
Fighter-bomberFighter
Generation
3rd generation3rd generation
National Origin
United StatesSoviet Union
Manufacturer
McDonnell DouglasMikoyan-Gurevich
Price (USD)
$3 Million$6 Million
Primary Users
US NavySoviet Air Forces
First Flight
19581967
Last Production Year
19811985
# Units Built
5,1955,047
Status
RetiredLimited Service
Seats
21
Length
19 m63 ft
16 m54 ft
Wingspan
11 m38 ft
14 m45 ft
Wing Area
49 m²529 ft²
37 m²402 ft²
Height
5 m16 ft
4 m15 ft
Empty Weight
13,757 kg30,330 lbs
10,886 kg24,000 lbs
Gross Weight
18,824 kg41,500 lbs
14,842 kg32,720 lbs
MTOW
28,030 kg61,795 lbs
17,799 kg39,240 lbs
Fuel Capacity
7,257 kg16,000 lbs
4,672 kg10,300 lbs
Number of Engines
21
Engine Type
TurbojetTurbojet
Engine Manufacturer
General ElectricKhatchaturov
Engine Model
J79-GE-17AR-35-300
Dry Thrust
53 kN11,905 lbs
84 kN18,800 lbs
Thrust w/ Afterburner
79 kN17,845 lbf
127 kN28,660 lbf
Max Thrust
159 kN35,690 lbf
127 kN28,660 lbf
Max Speed (Mach)
Mach 2.23Mach 2.35
Top Speed
2,371 km/h1,473 mph
2,499 km/h1,553 mph
Range
2,815 km1,520 nm
1,852 km1,000 nm
Rate of Climb
208 m/s41,000 ft/min
229 m/s45,000 ft/min
Ceiling
17,069 m56,000 ft
18,501 m60,700 ft
G Limit
6 g7 g

What Are the Differences Between the F-4 Phantom II and MiG-23

F-4 Phantom II vs MiG-23 Size Comparison

  • At 19.20 meters, the F-4 Phantom II is 2.50 meters longer than the MiG-23.
  • With a wingspan of 14 meters, the MiG-23 is 2.30 meters wider from wingtip to wingtip.
  • The wing area of the F-4 Phantom II is 0.20 meters bigger than that of the MiG-23’s 4.80 meters.

F-4 Phantom II vs MiG-23 Price

  • The MiG-23 is more expensive than the F-4 Phantom II, with a unit cost of approximately 6 million compared to the F-4 Phantom II’s unit cost of approximately 3 million.

F-4 Phantom II vs MiG-23 Speed

  • The MiG-23 has a top speed of 1,553 miles per hour, and the F-4 Phantom II has a top speed of 1,473 miles per hour. Head to head, this makes the MiG-23 80 miles per hour faster than the F-4 Phantom II.

About the F-4 Phantom II

The McDonnell Douglas F-4 Phantom II is one of the most significant fighter jets in military aviation history, known for its versatility, powerful performance, and distinctive appearance. Initially developed for the US Navy in the late 1950s, the F-4 Phantom II set numerous speed and altitude records for its time and was later adopted by the U.S. Marine Corps and the U.S. Air Force.

Production History: The F-4 Phantom II was designed to meet the U.S. Navy's need for a supersonic fighter capable of carrying a significant payload over long distances, without sacrificing speed and maneuverability. The aircraft saw extensive combat in the Vietnam War, serving in both ground-attack and air superiority roles. Production ran from 1958 to 1981, with over 5,000 units built, making it one of the most produced American supersonic military aircraft.

Design Features: Characterized by its large size, twin engines, and tandem two-seat configuration, the F-4 Phantom II was designed without an internal cannon in its initial versions, relying instead on missiles for air combat. The F-4's distinctive design included drooping tail fins and diagonal tail wings, contributing to its recognizable silhouette.

Operational History: The F-4 Phantom II saw extensive use in the Vietnam War, where it performed admirably in dogfighting against lighter North Vietnamese aircraft, as well as in bombing missions. It was also a key figure in American air power throughout the Cold War. The F-4 served with distinction in later conflicts such as the Persian Gulf War and remained in use by several countries into the 21st century.

Comparison with Similar Models:

F-4 Phantom II vs. F-105 Thunderchief

Role and Capabilities: Both aircraft were critical to the U.S. Air Force during the Vietnam War. The F-105 was primarily used for deep strike bombing missions, while the F-4 served in a wider range of roles, including air superiority, fleet defense, and reconnaissance.

Performance: The F-105 Thunderchief, known as the "Thud," was the faster of the two at low altitude and carried a larger bomb load for ground-attack missions. However, the F-4 Phantom II's superior agility, higher service ceiling, and ability to operate from carriers made it a more adaptable and formidable aircraft.

F-4 Phantom II vs. MiG-21

Design: The MiG-21 was the Soviet Union's counterpart to the F-4 during the Vietnam War. It was smaller, lighter, and offered greater agility, designed primarily for air superiority with a secondary ground-attack capability. In contrast, the F-4 was a larger, more versatile fighter-bomber that could engage targets at longer ranges with its superior radar and missile armament.

Operational Capabilities: The MiG-21's agility made it a formidable adversary in visual range dogfights, while the F-4's powerful engines, advanced avionics, and diverse weapons loadout gave it an edge in beyond-visual-range engagements and multirole missions.

About the MiG-23

The Mikoyan-Gurevich MiG-23, known by its NATO reporting name "Flogger," is a third-generation jet fighter developed by the Soviet Union in the late 1960s. The MiG-23 was designed to meet the need for a more versatile and capable fighter, capable of achieving Mach 2.35 speeds, and was introduced as a successor to the MiG-21. It served in various roles, including interceptor, ground-attack, and scouting.

Production History: The MiG-23 was introduced into service with the Soviet Air Forces in 1970. Over its production life, which spanned two decades, more than 5,000 units were built, making it one of the most produced fighter aircraft of its time. The MiG-23 was exported widely, serving in the air forces of over 30 countries, and saw action in numerous conflicts during the latter half of the 20th century.

Design Features: The MiG-23's most notable feature is its swing-wing design, which allows the wings to be set at different angles to optimize performance at various speeds. At lower speeds, the wings could be extended for better lift and maneuverability, while at higher speeds, they could be swept back to reduce drag. The aircraft was powered by a single large turbojet engine, equipped with an afterburner for additional thrust.

Operational History: The MiG-23 saw combat in several Middle Eastern conflicts, including the Yom Kippur War, the Iran-Iraq War, and the Syrian Civil War. It was used extensively by the Soviet Union in Afghanistan during the 1980s, where it was employed in both air-to-air combat and ground-attack roles. Despite its advanced design, the MiG-23 faced challenges in terms of maintenance and operational readiness, particularly in the hands of less experienced air forces.

Comparison with Similar Models:

MiG-23 vs. F-4 Phantom II

Role and Capabilities: Both the MiG-23 and F-4 Phantom II were designed as multi-role fighters capable of performing both air superiority and ground-attack missions. The MiG-23's variable-geometry wings provided it with a broader performance envelope, especially in terms of speed and altitude capabilities.

Performance: The F-4 Phantom II, while older, was known for its reliability, heavy payload, and versatility. In contrast, the MiG-23 offered better agility at high speeds and a more sophisticated radar and missile armament for air-to-air engagements.

MiG-23 vs. F-14 Tomcat

Design Evolution: The F-14 Tomcat and the MiG-23 were both developed around the same time and featured variable-geometry wings. This design was chosen by both manufacturers for similar reasons: to provide excellent performance across a wide range of speeds and altitudes.

Operational Capabilities: The F-14 was primarily designed as a fleet defense interceptor for the U.S. Navy and excelled in long-range air-to-air engagements. The MiG-23, while also capable in the interceptor role, was more versatile, being used extensively in ground-attack missions in addition to air superiority roles.

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Values shown may not be 100% accurate, as some metrics are averages or only represent certain production years and configurations. Engine specs are based on the best options available.

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