AGM-154 Joint Standoff Weapon [JSOW]
| Specifications | |||
|---|---|---|---|
| Mission | Close air support, interdiction, amphibious strike and anti-surface warfare | ||
| Variants |
AGM-154A Baseline |
AGM-154B Anti-Armor |
AGM-154C Unitary |
| Service | Navy and Air Force | Navy and Air Force | Navy |
| Contractor | Raytheon [Texas Instruments] | ||
| Targets | Mobile soft, fixed soft | Mobile hard, mobile soft | Fixed hard, maritime surface |
| First capability | 1997 | 2004 | |
| Guidance method | GPS/INS | JSOW
airframe -- GPS/INS
BLU-108 submunitions -- two-color infrared sensors |
GPS/INS with a terminal seeker and man- in-the-loop data link |
| Range |
12 nm (24km) Low altitude launch (unpowered) 40 nm (64 km) High altitude launch (unpowered) 120 nm (200 km) Powered | ||
| Weight | From 1065 pounds (483 kilograms) to 1500 pounds (681 kilograms) depending upon the payload, sensor and propulsion combination. | ||
| Circular Error Probable | |||
| Development cost | $417.9 million | $227.8 million | $452.4 million |
| Production cost | $2,909.7 million | $1,805.7 million | $5,155.9 million |
| Total acquisition cost | $3,327.6 million | $2,033.5 million | $5,608.3 million |
| Acquisition unit cost | $282,000 | $484,167 | $719,012 |
| Production unit cost | $246,585 | $429,929 | $661,013 |
| Quantity | Navy: 8,800; Air Force: 3,000 |
Air Force: 3,000 |
Navy 7,800 |
| Platforms | B-1, F-16, F-15E, F/A-18C/D, F/A-18E/F, AV-8B, P-3, S-3 | B-1, F-16 C/D, F-15E, F/A-18C/D, F/A-18E/F, AV-8B, P-3, S-3 | F/A-18C/D, F/A-18E/F, AV-8B, P-3, S-3 |
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