The Vympel R-73 was developed to replace the earlier R-60 (AA-8 'Aphid') weapon for short-range use by Soviet fighter aircraft. Work began in 1973, and the first missiles entered service in 1982.
The Vympel R-73 is an infrared-guided (heat-seeking) missile with a sensitive, cryogenic cooled seeker with a substantial "off-boresight" capability: the seeker can "see" targets up to 60° off the missile's centerline. It can be targeted by a helmet-mounted sight (HMS) allowing pilots to designate targets by looking at them. Minimum engagement range is about 300 meters, with maximum aerodynamic range of nearly 30 km (18.75 mi) at altitude.
The Vympel R-73 is a highly maneuverable missile and mock dogfights have indicated that the high degree of "off-boresight" capability of the R-73 would make a significant difference in combat. The missile also has a mechanically simple but effective system for thrust-vectoring. Altogether this prompted the development of the Sidewinder and other SRM successors like AIM-132 ASRAAM, IRIS-T, MICA IR, Python IV and the latest Sidewinder variant, AIM-9X, that entered squadron service in 2003.
From 1994 the R-73 has been upgraded in production to the R-73M standard, which entered CIS service in 1997. The R-73M has greater range and a wider seeker angle (to 60° off-boresight), as well as improved IRCCM (Infra-Red Counter-Counter-Measures).
An improved version of the R-73M, the R-74M features fully digital and re-programmable systems, and is intended for use on the MiG-35 or MiG-29K/M/M2 and Su-27SM, Su-30MK and Su-35BM.
The weapon is used by the MiG-29, MiG-31, Su-27, Su-34 and Su-35, and can be carried by newer versions of the MiG-21, MiG-23, Sukhoi Su-24, and Su-25 aircraft. India is looking to use the missile on their HAL Tejas. It can also be carried by Russian attack helicopters, including the Mil Mi-24, Mil Mi-28, and Kamov Ka-50.
| Vympel R-73 | |
|---|---|
| Type | short-range air-to-air missile |
| Place of origin | Soviet Union |
| Service history | |
| In service | 1982-present |
| Production history | |
| Manufacturer | Vympel |
| Specifications | |
| Weight | 105 kilograms (230 lb) |
| Length | 2.93 metres (9 ft 7 in) |
| Diameter | 165 millimetres (6.5 in) |
| | |
| Warhead | 7.4 kilograms (16 lb) |
| | |
| Engine | solid-fuel rocket engine |
| Wingspan | 510 millimetres (20 in) |
| Operational range | R-73E: 20 kilometres (12 mi) R-73M1: 30 kilometres (19 mi) R-73M2: 40km (24.7 miles) |
| Speed | Mach 2.5 |
| Guidance system | All-aspect infrared homing |
| Launch platform |
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