Vympel R-23

The Vympel R-23 (NATO reporting name AA-7 "Apex") is a medium-range air-to-air missile developed by the Soviet Union for fighter aircraft. An updated version with greater range, the R-24, replaced it in service. It is comparable to the American AIM-7 Sparrow, both in terms of overall performance as well as role.

Development

Design of a new missile to arm the MiG-23 fighter started in the mid-1960s under the direction of V.A. Pustyakov's design team. Known as the K-23 during its design, the new weapon was intended for use against bomber-sized targets, with "snap-up" capability to attack targets at higher altitude than the launch aircraft. It originally was intended to have a dual-mode seeker using both semi-active radar homing and infrared guidance, but this proved unfeasible, and separate SARH and IR models ("zdeliye" (Product) 340 and 360, respectively) were developed instead. Test firings were carried out in 1967, although the SARH missile's seeker head proved to be extremely problematic.

In 1968 the Soviets acquired an AIM-7M and a Vympel team started copying it as the K-25. A comparison of the two led to the K-23 entering production, based largely on its better range and countermeasures resistance. The K-25 work ended in 1971. Nevertheless, several features of the Sparrow were later used in the Vympel R-27 design.

The missile, designated R-23, entered service in January 1974, the SARH version as the R-23R, the IR version R-23T. Both versions used the same motor and warhead, which had a lethal radius of 8 m (26 ft). In the west these were known as the AA-7A and AA-7B, respectively. An inert training round, the R-23UT, was also developed.

The airframe featured four delta wings arranged cruciform just behind the midpoint of the fuselage, and cropped-delta control surfaces at the extreme rear in-line with the wings. Smaller cropped-triangular surfaces are mounted in-line near the nose (their purpose is unclear). The only external difference between the two versions was the nose cone, which was an ogive for the SAHR seeker, and shorter (by 30 cm) and more rounded for the IR version.

Maximum effective range for the R-23R was about 14 km (8.8 mi) at low level and 25 km (15.6 mi) at high altitude. The range for the R-23T was about 11 km (6.9 mi), limited by the visual-range needs of its seeker, not the motor. Both could be launched with the aircraft maneuvering at up to 4"g" against a target maneuvering at up to 5"g". One of its greatest tactical limitations was its lengthy minimum range, which was 1,300 m (4,160 ft) for a rear engagement, and up to 2 km for the SAHR version.

Large numbers of R-23s were built., both by Molniya (ex OKB-4) as well as Vympel (ex OKB-134). The R-23 was also produced under license in Romania as the A-911.

Starting in 1975 an improved version of the weapon was developed to arm the MiG-23ML/MLD. The resultant SAHR R-24R had lock-on after launch capability and expanded range (up to 50 km) and altitude capability (up to 25,000 m/82,000 ft), while the IR R-24T had a much improved seeker with greater sensitivity. Both versions had a larger motor, a heavier warhead, and a greatly reduced minimum range of 500 m (1,600 ft) for a rear-quarter engagement. They also could be used by or against aircraft maneuvering at up to 7"g". The missiles were known officially as "izdeliye" (Product) 140 and 160 in the USSR, and AA-7C and AA-7D in the west.

The R-24 remained in at least limited Russian service until the withdrawal of the last Russian MiG-23s in 1997.

Combat Record

The R-23 was used in the Beqaa Valley in June 1982, during the 1982 Lebanon War. However, it is hard to judge its success. Soviet and Syrian sources claim that it achieved a few kills while the Israelis deny this.

Many R-23 kills are reported in the war between Iran and Iraq when Iraqi MiG-23s fired them at Iranian F-4D/Es and F-5Es.

pecifications

* Length: (R-23R, R-24R) 4.5 m (14 ft 9 in); (R-23T, R-24T) 4.2 m (13 ft 9 in)
* Wingspan: 1 m (3 ft 5 in)
* Diameter: 223 mm (8.8 in)
* Launch weight: (R-23R, R-24R) 222 kg (489 lb), 243 kg (536 lb); (R-23T, R-24T) 215 kg (474 lb), 235 kg (518 lb)
* Speed: Mach 3
* Range: (R-23R) 35 km (22 mi); (R-24R) 50 km (31 mi); (R-23T, R-24T) 15 km (9.4 mi)
* Guidance: (R-23R, R-24R) SARH; (R-23T, R-24T), infrared-homing
* Warhead: expanding-rod high explosive with proximity fuze, 25 kg (55 lb) (R-23) or 35 kg (77 lb) (R-24)

References

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