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Sprint (missile)

Spacecraft and Launch Vehicles

The Sprint was a two-stage, solid-fuel anti-ballistic missile that Martin Marietta developed for the United States Army, armed with a W66 enhanced-radiation thermonuclear warhead. It was built to intercept incoming reentry vehicles after they had dropped below about 60 kilometres, where the thickening air exposed them to radar. To do that it accelerated at 100 g and reached Mach 10 in five seconds, which heated its skin enough to need an ablative shield and wrapped the missile in a plasma that made radio guidance difficult. Sprint was the close-in layer of the Nike-X, Sentinel and Safeguard missile defence plans, working beside the longer-ranged LIM-49 Spartan. Safeguard was operational for only a few months from October 1975 to early 1976, so Sprint served in 1975 and 1976. Some work on an improved Sprint II, mostly on guidance, was done in the early 1970s before United States anti-ballistic missile policy changed and it stopped.

Facts
Year
1975 2
Propulsion
Solid propellant 1
Engine Class
Rocket 2
Status
Retired from service 2
Comparison
Body Style
Missile 1
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Same As

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Source Designation-Systems.Net: Martin Marietta SprintHistory, development contract
Quote, History, development contract
Martin Marietta received a development contract for the Sprint missile in March 1963

Originated In

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Source Designation-Systems.Net: Martin Marietta SprintLead, American defense system
Quote, Lead, American defense system
one component of an American defense system against Soviet ICBMs
Sources
1. Sprint (missile) (Wikipedia)
  • Lead, vehicle kind
    The Sprint was a two-stage, solid-fuel anti-ballistic missile (ABM)
  • Lead, fuel
    solid-fuel anti-ballistic missile
View the Source
2. Designation-Systems.Net: Martin Marietta Sprint
Designation-Systems.Net
  • History, Safeguard site operational
    On 1 October 1975, the U.S.'s one and only Safeguard ABM site became operational with 30 LIM-49A Spartan and 70 Sprint missiles.
  • History, Safeguard site deactivated
    the site was deactivated by Congress the next day
  • Description, motor
    powered by a two-stage solid-propellant rocket motor
View the Source
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