Raduga K-9
| Raduga K-9 (Kaliningrad K 9) | |
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| General Information | |
| Type | Air-to-air missile |
| Manufacturer | MKB Fakel (design office P. D. Gruschin ) |
| development | 1958 |
| Commissioning | 1961 |
| Technical specifications | |
| length | 4.5 m |
| diameter | 250 mm |
| Combat weight | 245 kg |
| span | 1.6 m |
| drive | Solid rocket |
| speed | 5040 km / h |
| Range | 9 km |
| Furnishing | |
| Target location | Radar beacon guidance |
| Warhead | 27 kg |
| Weapon platforms | Fighter planes , specifically the Mikoyan-Gurevich Je-152 model |
| Lists on the subject | |
The Raduga K9 ( NATO code name : AA-4 Awl ) was a Soviet short-range air-to-air missile. It was developed by the Raduga design office in the late 1950s. The guided missile K-9 never went into series production.
Web links
- K-9 on airwar.ru (Russian)
literature
- Jefim Gordon : Soviet / Russian Aircraft Weapons Since World War Two . Midland, Hinckley 2004, ISBN 1-85780-188-1 .