| Specifications |
| Primary Function: | Air-to-surface anti-radiation missile
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Mission | Defense suppression
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Targets | Fixed soft
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Service | Navy and Air Force
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| Contractor: | Raytheon [Texas Instruments]
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Program status | Operational
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| Date Deployed: | 1984
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| Power Plant: | Thiokol dual-thrust rocket motor
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| Thrust: | Dual thrust
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| Length: | 13 feet, 8 inches (4.14 meters)
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| Launch Weight: | 800 pounds (360 kilograms)
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| Diameter: | 10 inches (25.40 centimeters)
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| Wingspan: | 3 feet, 8 inches (101.60 centimeters)
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| Range: | 30 plus miles (48 plus kilometers)
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| Speed: | Max. speed: 2280 km/h
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| Guidance System: | Proportional
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| Guidance method | Homes on electronic emissions
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| Warhead | WAU-7/B, 143.51bs. Direct Fragmentation |
| Explosive (NEW) | PBXC-116 (45.2 lbs.) |
| Fuze | Pulsed Laser Proximity/Contact |
| Propulsion | Boost Sustain 64,000 lbs./sec. Low Smoke |
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Development cost | $644.5 million
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Production cost | $5,568.1 million
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|
Total acquisition cost | $6,212.6 million
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Acquisition unit cost | $316,856
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Production unit cost | $283,985
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Quantity | 19,607 (Navy and Air Force)
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Platforms | F/A-18, A-6E, F-4G, F-16
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