| AGM-130 | |
|---|---|
 | |
| Type | Air-to-surface guided missile |
| Place of origin | United States |
| Service history | |
| In service | 1994–2013 |
| Used by | United States (USAF) |
| Wars | Kosovo War |
| Production history | |
| Unit cost | Approximately $450,000 per weapon[1] |
| Specifications | |
| Mass | 2,917 lb (1,323 kg) |
| Length | 12 feet, 10.5 inches (3.90 meters)[1] |
| Diameter | 15 in/18 in (38 cm/46 cm) (bomb); 9 in (23 cm) (rocket motor) |
| Wingspan | 59 in (150 cm) |
| Warhead | 2,000 lb (907 kg) BLU-109 or MK 84 |
Operational range | 46.6 miles (75 kilometers)[2] although exact range is classified[1] |
| Flight ceiling | 30,000-plus feet (9,100 meters) |
| Maximum speed | High subsonic,[3] but exact speed is classified[1] |
The AGM-130 was an air-to-ground guided missile developed by the United States of America. Developed in 1984, it is effectively a rocket-boosted version of the GBU-15 bomb. It first entered operational service on 11 January 1999, and was retired in 2013. 502 were produced.
- ^ a b c d "AGM-130 Missile". af.mil. Archived from the original on 6 September 2015. Retrieved 27 October 2015.
- ^ "AGM-130C (IR)". deagel.com. Archived from the original on 23 October 2015. Retrieved 27 October 2015.
- ^ "Boeing AGM-130". designation-systems.net. Archived from the original on 23 September 2015. Retrieved 27 October 2015.