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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