SS-N-3 Shaddock
| SS-N-3 Shaddock/Sepal | |
|---|---|
A P-5 missile on static display, red air intake cover clearly visibile | |
| Type | Cruise missile |
| Place of origin | Soviet Union |
| Service history | |
| In service | 1963−1991 (USSR) |
| Used by | See operators |
| Wars | Russo-Ukrainian War |
| Production history | |
| Designer | Chelomey Design Bureau |
| Variants | See variants |
| Specifications | |
| Mass | 5,300 kg (11,700 lb) |
| Height | 10.8 m (35 ft) |
| Diameter | 0.98 m (3 ft 3 in) |
| Wingspan | 2.5 m (8 ft 2 in) |
| Warhead | HE SAP or nuclear |
| Warhead weight | 650 or 870 kg (1,430 or 1,920 lb) |
| Blast yield | 10 or 200 kt |
| Engine | Turbojet with solid fuel boosters |
| Propellant | Liquid fuel |
Operational range | 300 or 450 km (190 or 280 mi) |
| Maximum speed | 1.3 Mach |
Guidance system | Inertial with commands and infrared or active radar |
Launch platform | |
| References | |
The P-5 Pityorka (Russian: П-5 «Пятёрка», lit. 'five'), also known by the NATO reporting name SS-N-3 Shaddock for submarine-launched versions and SS-N-3 Sepal for ship and coastal defence versions, is a Cold War era turbojet-powered cruise missile of the Soviet Union, designed by the Chelomey design bureau. Originally designed as a strategic nuclear weapon, it entered service in 1963 with the Soviet Navy. All ship and submarine launched versions remained in service until 1994, while coastal defence batteries remain in limited service with the Russian Navy.