RIM-24 Tartar
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RIM-24 Tartar | |
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RIM-24 Tartar | |
Basic data | |
Function | medium range surface-to-air missile |
Manufacturer | General Dynamics (Convair) |
Entered service | 1962 |
General characteristics | |
Engine | Dual thrust, Solid-fuel rocket |
Launch mass | 1310 lb |
Length | 180 in |
Diameter | 13.5 in |
Speed | Mach 1.8 |
Range | 8.7 nm (RIM-24A) 16 nm (RIM-24B) 17.5 nm (RIM-24C) |
Service ceiling | 50,000ft (RIM-24A) 65,000ft (-24B) |
Warhead | 130 lb continuous-rod |
Guidance | SARH |
Launch platform | Surface Ship |
The General Dynamics RIM-24 Tartar was a medium-range naval surface-to-air missile (SAM), and was among the earliest surface-to-air missiles to equip United States Navy ships. The Tartar was the third of the so-called "3 T's", the three primary SAMs the Navy fielded in the 60s and 70s, the others being the RIM-2 Terrier and RIM-8 Talos.
[edit] History
The Tartar was born of a need for a more lightwieght system for smaller ships, and something that could engage targets at very close range. Essentially, the Tartar was simply a RIM-2C Terrier without the secondary booster. The Tartar was never given a SAM-N-x designation, and was simply referred to as Missile Mk 15 until the RIM designation system was introduced in 1963.
The Tartar was used on a number of ships, of a variety of sizes. Initially the Mk 11 twin-arm launcher was used, later ships used the Mk 13 and Mk 22 single-arm launchers.
The Tartar was replaced in U.S. Navy service with the RIM-66 Standard Missile (MR). Even after the upgrade to a new missile, ships were still said to be Tartar ships because they carried the Tartar Guided Missile Fire Control System.
[edit] Variations
- RIM-24A - Original missile
- RIM-24B - Improved Tartar
- RIM-24C - Improved Tartar Retrofit (ITR) aka. Tartar Reliability Improvement Program (TRIP)