AGM-88 HARM
Specifications | |
---|---|
Primary Function: | Air-to-surface anti-radiation missile |
Mission | Defense suppression |
Targets | Fixed soft |
Service | Navy and Air Force |
Contractor: | Raytheon [Texas Instruments] |
Program status | Operational |
Date Deployed: | 1984 |
Power Plant: | Thiokol dual-thrust rocket motor |
Thrust: | Dual thrust |
Length: | 13 feet, 8 inches (4.14 meters) |
Launch Weight: | 800 pounds (360 kilograms) |
Diameter: | 10 inches (25.40 centimeters) |
Wingspan: | 3 feet, 8 inches (101.60 centimeters) |
Range: | 30 plus miles (48 plus kilometers) |
Speed: | Max. speed: 2280 km/h |
Guidance System: | Proportional |
Guidance method | Homes on electronic emissions |
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 |
Development cost | $644.5 million |
Production cost | $5,568.1 million |
Total acquisition cost | $6,212.6 million |
Acquisition unit cost | $316,856 |
Production unit cost | $283,985 |
Quantity | 19,607 (Navy and Air Force) |
Platforms | F/A-18, A-6E, F-4G, F-16 |
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