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LIM-49A Spartan

LIM-49A Spartan
Type Anti-ballistic missile
Place of origin United States
Service history
In service 1975
Production history
Manufacturer Western Electric & McDonnell Douglas
Specifications
Weight 29,000 lb (13,100 kg)
Length 55 ft 2 in (16.8 m)
Diameter 3 ft 7 in (1.08 m)
Warhead W71 nuclear; 5 Mt

Engine 1st Stage: Thiokol TX-500 (2200 kN);
2nd Stage: Thiokol TX-454;
3rd Stage: Thiokol TX-239
Wingspan 9 ft 9.6 in (2.98 m)
Operational
range
460 mi (740 km)
Flight altitude 350 mi (560 km)
Speed >Mach 4
Guidance
system
Radio command
Launch
platform
Silo

The LIM-49A Spartan was a United States Army anti-ballistic missile, designed to intercept attacking nuclear warheads from Intercontinental ballistic missiles at long range and while still outside the atmosphere. For actual deployment, a five-megaton thermonuclear warhead was planned to destroy the incoming ICBM warheads. It was part of the Safeguard Program.

Spartan was the latest and, as it turned out, final development in a long series of missile designs from the team of Bell Laboratories and Douglas Aircraft Company that started in the 1940s with the Nike. Spartan was developed directly from the preceding LIM-49 Nike Zeus, retaining the same tri-service identifier, but growing larger and longer ranged, from the Zeus' 250 nautical miles (460 km) to approximately 450 nautical miles (830 km).

Spartan was initially developed as part of the Nike-X project, later becoming the Sentinel Program. This was eventually cancelled and replaced with the much smaller Safeguard Program. Spartans were deployed as part of the Safeguard system from October 1975 to early 1976.

The US Army started their first serious efforts in the anti-ballistic missile arena when they asked the Bell Labs missile team to prepare a report on the topic in February 1955. The Nike team had already designed the Nike Ajax system that was in widespread use around the US, as well as the Nike Hercules that was in the late stages of development as the Ajax's replacement. They returned an initial study on Nike II in January 1956, concluding that the basic concept was workable using a slightly upgraded version of the Hercules missile, but requiring dramatically upgraded radars and computers to handle interceptions that took place at thousands of miles an hour.


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