| Specifications |
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Primary Function: | Air-to-surface strategic missile
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Contractor: | Boeing Aerospace Co.
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Guidance Contractors: | Litton Guidance and Control
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Power Plant: | Williams Research Corp. F-107-WR-10 turbofan engine
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Thrust: | 600 pounds (270 kilograms)
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Length: | 20 feet, 9 inches (6.29 meters)
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Weight: | 3,150 pounds (1,417.5 kilograms)
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Diameter: | 24.5 inches (62.23 centimeter)
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Wingspan: | 12 feet (3.64 meters)
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Range: | AGM-86B: 1,500-plus miles (1,305 nautical miles)
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Speed: | About 550 mph (Mach 0.73)
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Guidance System: | Litton inertial navigation element with terrain contour-matching updates
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Warheads: | W80-1 with a yield of 5 and 150 kt
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Sensors: | A terrain contour-matching guidance system that allows the missile to fly complicated routes to a target through use of maps of the planned flight route stored in on-board computers
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Unit Cost: | $1 million
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Date Deployed: | December 1982
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Inventory: | Active force, 1,628; ANG, 0; Reserve, 0
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