AGM-123 Skipper II
From Infogalactic: the planetary knowledge core
| AGM-123 Skipper II | |
|---|---|
| 300px | |
| Type | Rocket assisted, low-level, laser-guided bomb |
| Place of origin | United States |
| Service history | |
| In service | 1985 |
| Production history | |
| Manufacturer | Emerson Electric |
| Specifications | |
| Weight | 582 kg (1,283 lb) |
| Length | 4.3 m (14 ft 1.2 in) |
| Diameter | 0.5 m (1 ft 7.6 in) |
| Warhead | 1000 lb (450 kg) MK 83 bomb |
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| Engine | Aerojet MK 78 dual-thrust solid-fueled rocket |
| Wingspan | 1.6 m (5 ft 3 in) |
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Operational
range |
25 km (15.5 statute miles) |
| Speed | Max:1,100 km/h (680 mph) |
AGM-123 Skipper II is a short-range laser-guided missile developed by the United States Navy. The Skipper was intended as an anti-ship weapon, capable of disabling the largest vessels with a 1,000-lb (450-kg) impact-fuzed warhead.
It is composed of a Mark 83 bomb fitted with a Paveway guidance kit and two Mk 78 solid propellant rockets that fire upon launch. The rockets allow the munition to be dropped farther away from the target than could free-fall bombs, which helps protect the delivery aircraft from surface-to-air-missiles and anti-aircraft artillery near the target.
The AGM-123 was developed at the China Lake Naval Weapons Center and carried by the A-6E Intruder, A-7 Corsair II, and F/A-18.
External links
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Wikimedia Commons has media related to AGM-123 Skipper II. |
- Designation systems - Emerson Electric AGM-123 Skipper II
- Federation of American Scientists - AGM-123 Skipper II
