AGM-130
| AGM-130 | |
|---|---|
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| Type | Air-to-surface guided missile |
| Place of origin | United States |
| Service history | |
| In service | 1994–2013 |
| Used by | United States |
| Wars | Kosovo War |
| Production history | |
| Unit cost | Approximately $450,000 per weapon |
| Specifications | |
| Weight | 2,917 lb (1,323 kg) |
| Length | 12 feet, 10.5 inches (3.90 meters) |
| Diameter | 15 in/18 in (38 cm/46 cm) (bomb); 9 in (23 cm) (rocket motor) |
| Warhead | 907 kg (2,000 lb) BLU-109 or MK 84 |
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| Wingspan | 59 in (150 cm) |
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Operational
range |
46.6 miles (75 kilometers) although exact range is classified |
| Flight ceiling | 30,000-plus feet (9,100 meters) |
| Speed | high subsonic, but exact speed is classified |
46.6 miles (75 kilometers)
The AGM-130 is a powered air-to-ground guided missile developed by the United States of America. It is basically a rocket-boosted version of the GBU-15 bomb. Development of the AGM-130A began in 1984. It first entered operational service on 11 January 1999. 502 were produced.
The AGM-130 is a powered air-to-surface missile designed for strikes at long range against various targets. It is essentially a rocket-boosted version of the GBU-15 bomb, with the rocket motor increasing the launch range and so giving the launch aircraft protection from whatever defenses may protect the target. Two can be carried by the F-111 and F-15E.
The weapon utilizes inertial navigation aided by the Global Positioning System (GPS). It can be retargeted in flight; the guidance head of the weapon provides a visual image of the target to the launch aircraft via the AXQ-14 data link, allowing the controller to steer it to the target (command guidance). The weapon can be retargeted in flight by simply steering it to a new target. Control can be released at any point, allowing the missile to home in on the target by itself. The AGM-130 is highly accurate, and is intended for use against high-value targets which are either slow moving or of fixed location.
The GBU-15 is a modular weapon, and the AGM-130 continues this concept. It consists of a CCD TV or focal plane array imaging infrared seeker head, a radar altimeter, wings, strakes, a Mark 84 or BLU-109 warhead, a control section, and a rocket motor and data link unit.
The AGM-130 needs little support on the ground, and can be based in remote "bare base" sites. What support and maintenance is required can be provided by mobile support equipment and intermediate level maintenance capability.
Development of the AGM-130A began in 1984 as an improvement to the GBU-15. The first unit became operational in 1994. Precise numbers are classified, but the US Air Force planned to buy 4,000+ originally. This was reduced to 2,300 units, and in 1995 further reduced to 502.
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