AA-5 ASH
R-4
In 1959 the Bisnovat design team began work on the K-80 missile (Object 36 -- later called the R-40) as part of the the Tu-128S-4 interception system. This strategic air defense system consiste of the Tu-128 long-range interceptor fighter aircraft, a Smerch [Tornado] on-board radar set (the letter S in the system designation), and the R-4 missiles (the digit 4 in Tu-128S-4). Two variants of the R-4 missile were developed: the R-4R using a semiactive radar set with a PARG-10-88 homing head and the R-4T using infrared homing with the T-80NM seeker head. Apart from the Tu-128, only the Mikoyan E-152M experimental aircraft carried the R-4 missiles. The R-4 missile entered series-production in 1963, although significant development efforts remained, as was also the case with the Smerch radar set. In 1973 production began of the improved K-80M (R-4TM and R-4RM variants) for the Tu-128S-4M system, consisting of the Tu-128M aircraft, the Smerch-M radar set, and the R-4M missile. In the West the K-80 missile and its modifications are called The AA-5 Ash R-4 missile was withdrawn from service along with the remaining Tu-128 aircraft around the end of the Cold War.
| Specifications | |
|---|---|
| Contractor | |
| Year | 1961 |
| Type | medium-range missile |
| Modifications |
Infra-red guidance Semi-active radar guidance |
| Wingspan | 1.3 m |
| Length (SAR version) | 5.3 m |
| Length (IR version) | 5.2 m |
| Diameter | 0.31 m |
| Launch weight | 390 kg |
| Max. speed | 1710 km/h |
| Maximum range (SAR version) | 30 km |
| Maximum range (IR version) | 15 km |
| Propulsion | solid propellant rocket motor |
| Guidance | passive infra-red homing with Cassagrain optics or semi-active I-band radar homing |
| Warhead | high-explosive blast |
| Carried by | Tu-128 |
| Service | USSR, Czechoslovakia, Romania, Bulgaria, East Germany, Poland. |
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