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MIM-23 Hawk | |
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Type | Surface-to-air missile |
Place of origin | United States |
Service history | |
In service | August 1960[1]–present |
Wars | |
Production history | |
Manufacturer | Raytheon Company |
Specifications | |
Mass | 1,290 pounds (590 kg) |
Length | 16 feet 8 inches (5.08 m) |
Diameter | 14.5 inches (370 mm) |
Wingspan | 3 feet 11 inches (1.19 m) |
Warhead | 119 pounds (54 kg) blast fragmentation warhead |
Engine | solid-fuel rocket engine |
Operational range | 28–31 mi (45–50 km) |
Flight ceiling | 65,000 feet (20,000 m) |
Maximum speed | Mach 2.4 |
Guidance system | Semi-active radar homing |
The Raytheon MIM-23 HAWK ("Homing All the Way Killer")[2] is an American medium-range surface-to-air missile. It was designed to be a much more mobile counterpart to the MIM-14 Nike Hercules, trading off range and altitude capability for a much smaller size and weight. Its low-level performance was greatly improved over Nike through the adoption of new radars and a continuous wave semi-active radar homing guidance system. It entered service with the US Army in 1959.
In 1971 it underwent a major improvement program as the Improved Hawk, or I-Hawk, which made several improvements to the missile and replaced all of the radar systems with new models. Improvements continued throughout the next twenty years, adding improved ECCM, a potential home-on-jam feature, and in 1995, a new warhead that made it capable against short-range tactical ballistic missiles. Jane's reported that the original system's single shot kill probability was 0.56; I-Hawk improved this to 0.85.[3]
Hawk was superseded by the MIM-104 Patriot in US Army service by 1994. The last US user was the US Marine Corps, who used theirs until 2002 when they were replaced with the man-portable short-range FIM-92 Stinger. The missile was also produced outside the US in Western Europe, Japan and Iran.[4] The US never used the Hawk in combat, but it has been employed numerous times by other nations. Approximately 40,000 of the missiles were produced.