AGM-123 Skipper II | |
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Type | Rocket assisted, low-level, laser-guided bomb |
Place of origin | United States |
Service history | |
In service | 1985-current |
Production history | |
Manufacturer | Emerson Electric |
Specifications | |
Mass | 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) |
Operational range | 25 km (15.5 statute miles) |
Maximum 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.
Operational history[]
Four Skipper missiles launched by A-6E Intruders contributed to sinking the Iranian frigate Sahand during Operation Praying Mantis on April 18, 1988.[citation needed]
Skipper missiles were also fired in Operation Desert Storm against Iraqi surface vessels by A-6s and U.S. Marine aircraft.[citation needed]
External links[]
Wikimedia Commons has media related to Category:AGM-123 Skipper II. |
- Designation systems - Emerson Electric AGM-123 Skipper II
- Federation of American Scientists - AGM-123 Skipper II
The original article can be found at AGM-123 Skipper II and the edit history here.