(NATO reporting name: SS-N-19 'Shipwreck')
|Type||Long-range anti-ship cruise missile|
|Place of origin||Soviet Union/Russia|
|In service||Since 1983|
|Used by||Soviet Union, Russia|
|Designer||OKB-52/NPO Mashinostroyeniya Chelomey|
|Weight||7,000 kg (15,400 lb)|
|Length||10 m (33 ft)|
|Diameter||0.85 m (33 in)|
|Warhead||High explosive or nuclear|
|Warhead weight||750 kg (1,653 lb) HE (unknown composition, probably RDX or similar) or 500 kt fission-fusion thermonuclear weapon|
|Blast yield||500 kt|
|625 km (388 mi)|
|Speed||Mach 1.6 (low altitude) - 2.5+ (high altitude)|
|Inertial guidance, active radar homing with home-on-jam, and Legenda satellite targeting system (believed to be nonfunctional after the fall of the USSR)|
|Oscar class submarines
Kirov & Admiral Kuznetsov class ships
The P-700 Granit (Russian: П-700 "Гранит"; English: granite) is a Soviet and Russian naval anti-ship cruise missile. Its GRAU designation is 3M45, its NATO reporting name SS-N-19 Shipwreck. It comes in surface-to-surface and submarine-launched variants , modern version is P-1200 Bolid GRAU code 3M-15 AShM SLCM .
Design and building
The P-700 was designed in the 1970s to replace the P-70 Ametist and P-120 Malakhit, both effective missiles but with too short a range in the face of improving weapons of U.S. Navy carrier battle groups. The missile was partially derived from the P-500 Bazalt.
Built by Chelomei/NPO Mashinostroenia, the bulging 10m missile has swept-back wings and tail, weighs around 7,000 kilograms and can be fitted with either a 750 kg HE warhead, a FAE warhead, or a 500 kt nuclear warhead. A stubby cylindrical solid-fuel rocket is fitted to the rear for launch; this booster stage is released when the missile enters sustained flight. For many years it was believed that this missile used a turbojet engine during the sustained flight; after the Russian and the Western media gained access to its performance characteristics, it was understood that its propulsion system was a ramjet. The P-700 has a distinctive annular air intake in the nose. Maximum speed is believed to be between Mach 1.6 and more than Mach 2.5. Range is estimated at 500 to 550–625 km. The guidance system is mixed-mode, with inertial guidance, terminal active radar homing guidance with and also anti-radar homing. Mid-course correction is probable.
The missile, when fired in a swarm (group of 4–8) has a unique guidance mode. One of the weapons climbs to a higher altitude and designates targets while the others attack. The missile responsible for target designation climbs in short pop-ups, so as to be harder to intercept. The missiles are linked by data connections, forming a network. If the designating missile is destroyed the next missile will rise to assume its purpose. Missiles are able to differentiate targets, detect groups and prioritize targets automatically using information gathered during flight and types of ships and battle formations pre-programmed in an onboard computer. They will attack targets in order of priority, highest to lowest: after destroying the first target, any remaining missiles will attack the next prioritized target. Such description received some doubts. The missile has a means of countering the attacking anti-missiles. Also, onboard computer has data to counter the enemy's electronic warfare and tactics of evasion from the fire of air defense.
The P-700 was derived from the P-500 Bazalt missile with a turbojet. The P-700 was in turn developed into the P-800 Oniks, which uses ramjet propulsion, and the BrahMos missile, a joint Indian/Russian modernization of the P-800.
It is currently in service with the Russian Northern Fleet on the Kirov-class battlecruisers Admiral Nakhimov and Pyotr Velikyi, the aircraft carrier Kuznetsov, and with the Russian Northern and Pacific fleets as part of the armoury for the Oscar-class cruise missile submarines (the Kursk carried 24 missiles).
The size of the missile limits the platforms on which it can operate and be launched from.
The missile was partially derived from the P-500 and P-700. Maximum speed is believed to be between Mach 2 and more than Mach 2.5. Range is estimated at 700 to 1000 km (800). Warhead: 500 kg. Years of production 1985-1992. The body of the rocket resembles that of the P-500, but used the ability of the P-700 to overcome defensive countermeasures. Long range rocket flight can achieve the goal only at low altitudes (up to 25 meters or lower) approximation (in which case the maximum range is less than 500 km).
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