Vympel R-23

R-23 / R-24 AA-7 Apex
R-23T on Polish MiG-23
Type	Medium air-to-air missile
Place of origin	Soviet Union
Service history
In service	1974-1997
Used by	Soviet Air Forces, others
Production history
Designer	V. A. Pustyakov
Manufacturer	Vympel
Specifications (R-23R)
Weight	222 kg (489 lb)
Length	4.50 m (14 ft 9 in)
Diameter	223 mm (8.8 in)
Warhead	expanding-rod high explosive
Warhead weight	25 kg (55 lb)
Engine	solid fuel rocket
Propellant	1.04 m (3 ft 5 in)
Operational range	35 kilometres (22 mi)
Speed	Mach 3
Guidance system	semi-active radar homing (R-23R/R-24R) infrared homing (R-23T/R-24T)
Launch platform	MiG-23

The R-23 (NATO reporting name AA-7 Apex) is a medium-range air-to-air missile developed by Vympel in 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.

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-7 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 : known as "destabilizers", they serve to improve the rudders' efficiency at high angles of attack (the R-60 missile uses the same feature). The only external difference between the two versions was the nose cone, which was an ogive for the SARH seeker, and shorter (by 30 cm) and more rounded for the IR version.