Mikoyan-Gurevich MiG-23
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MiG-23
Type Fighter
Manufacturer Mikoyan-Gurevich OKB
Maiden flight 1967-06-10
Introduced 1970
Retired 1994, Russia
Remains in service with foreign users
Primary user Soviet Air Force
Produced 1967-1985
Number built 5,047
Variants MiG-27 'Flogger-D/-J'

The Mikoyan-Gurevich MiG-23 (Russian: Микоян и Гуревич МиГ-23; NATO reporting name: "Flogger") is a variable geometry, swept-wing fighter aircraft, originally built by the Mikoyan-Gurevich design bureau in the Soviet Union. Produced in large numbers, it remains in limited service with various export customers.
Contents
[hide]

* 1 Development
* 2 First-generation MiG-23s
o 2.1 Flogger-A
o 2.2 Flogger-B
o 2.3 Flogger-C
o 2.4 Flogger-E
* 3 Second-generation MiG-23s
o 3.1 Flogger-G
o 3.2 Flogger-K
* 4 Ground-attack variants
o 4.1 Flogger-F
o 4.2 Flogger-H
* 5 Proposed variants and upgrades
o 5.1 Price
* 6 Service career
* 7 Western and Israeli claims
o 7.1 Russian Claims
o 7.2 Performance Tests
o 7.3 Soviet & Warsaw Pact Service
* 8 Operators
o 8.1 Current Operators
o 8.2 Former Operators
* 9 Specifications (MiG-23MLD Flogger-L)
* 10 Footnotes
* 11 Trivia
* 12 External links
* 13 Related content

[edit] Development

The MiG-23's predecessor, the MiG-21 (NATO reporting name 'Fishbed'), was fast and agile, but limited in its operational capabilities by its primitive radar, short range, and limited weapons load (restricted in some aircraft to a pair of short-range air-to-air missiles). The MiG-23 was to be a heavier, more powerful machine designed to remedy these deficiencies, and, it was hoped, rival Western aircraft like the F-4 Phantom. The new fighter was to feature a totally new S-23 sensor and weapon system suite capable of firing beyond-visual-range (BVR) missiles.
MiG-23 on display at Le Bourget
MiG-23 on display at Le Bourget

A major design consideration was take-off and landing performance. The existing Soviet fast jets required very long runways, which combined with their limited range, limited their tactical usefulness. The Soviet Air Force demanded that the new aircraft have a much shorter take-off run. Low-level speed and handling was also to be improved over the MiG-21. This led Mikoyan to consider two alternatives: lift jets, to provide an additional lift component, and variable-geometry wings, which had been developed by TsAGI for both "clean-sheet" aircraft designs and adaptations of existing designs.

The first prototype, called "23-01" but also known as the MiG-23PD, was a tailed delta-wing design similar to the MiG-21 but with two lift jets in the fuselage. However, it became apparent very early that this configuration was unsatisfactory, as the lift jets became useless dead weight once airborne. The second prototype, known as "23-11", featured variable-geometry wings which could be set to angles of 16, 45 and 72 degrees, and it was clearly more promising. The maiden flight of 23-11 took place on June 10, 1967, and three more prototypes were prepared for further flight and system testing. All featured the Tumansky R-27-300 turbojet engine with a thrust of 7850 kg. The order to start series production of the MiG-23 was given in December 1967.

The General Dynamics F-111 and McDonnell Douglas F-4 were the main Western influences on the MiG-23. The Russians, however, wanted a much lighter, single-engine fighter to maximize agility. Both the F-111 and the MiG-23 were designed as fighters, but the heavy weight of the F-111 turned it into a long-range interdictor and kept it out of the fighter role. The MiG-23's designers kept the MiG-23 light enough to dogfight with enemy fighters.

The U.S. Air Force operated a small number of MiG-23s, which were officially designated the YF-113G as both test and evaluation aircraft and in an aggressor role for fighter pilot training, from 1977 through 1988 in a program code named "Constant Peg".[1]

[edit] First-generation MiG-23s

[edit] Flogger-A

* The Ye-231 was the prototype built for testing, and it lacked the sawtooth leading