||This article's lead section may not adequately summarize key points of its contents. (March 2011)|
|Type||Air-to-surface guided missile|
|Place of origin||United States|
|Used by||United States|
|Weight||2,917 lb (1,323 kg)|
|Length||154 in (390 cm)|
|Diameter||15 in/18 in (38 cm/46 cm) (bomb); 9 in (23 cm) (rocket motor)|
|Warhead||240 kg (530 lb) BLU-109 or 430 kg (950 lb) MK 84|
|Wingspan||59 in (150 cm)|
|more than 40 miles (60 kilometers)|
|Flight ceiling||30,000-plus feet (9,100 meters)|
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-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. 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.
Development of the AGM-130 cost $192 million, not including a further $11 million for the AGM-130C. Unit cost of the weapons are an estimated $880,000.
The upgraded AGM-130 Mid-Course Guidance (MCG) weapon, employs an improved global positioning and inertial navigation system. This allows the weapon to be used with less input from the launch aircraft, freeing the pilot and weapon systems officer for other tasks. The weapon became operational in 1998 when two F-15Es from the 335th and 336th Fighter Squadrons at Seymour Johnson Air Force Base, North Carolina, fired one weapon each.
The AGM-130LW [lightweight] is designed to be used by single-seat aircraft such as the F-16C/D. It also has an enhanced global positioning and inertial navigation system capability. The smaller, less powerful warhead used on this weapon allows better control over collateral damage.
The AGM-130C employed a 2,000-pound penetrating warhead for use against hardened targets. It was developed, but not put into service.
The Autonomous AGM-130 is a proposed weapon that would incorporate a laser radar (LADAR) seeker, removing any need for the weapon to be steered to the target. The aircraft interface would be based on the JDAM interface; use of the autonomous seeker would greatly reduce the mission planning requirements and aircrew workload. Elimination of the datalink would also reduce the susceptibility to countermeasures.
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