AGM-123 Skipper II

Summary

AGM-123 Skipper II
AGM-123 Skipper II.jpg
TypeRocket assisted, low-level, laser-guided bomb
Place of originUnited States
Service history
In service1985-1990s[1]
Production history
ManufacturerEmerson Electric
Specifications
Mass582 kg (1,283 lb)
Length4.3 m (14 ft 1.2 in)
Diameter0.5 m (1 ft 7.6 in)
Warhead1000 lb (450 kg) MK 83 bomb

EngineAerojet MK 78 dual-thrust solid-fueled rocket
Wingspan1.6 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 one Mk 78 solid propellant rocket that fires upon launch. The rocket 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]

References

  1. ^ "Emerson Electric AGM-123 Skipper II".

External links

  • Designation systems - Emerson Electric AGM-123 Skipper II
  • Federation of American Scientists - AGM-123 Skipper II