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AGM-123 Skipper II

From Wikipedia, the free encyclopedia

AGM-123 Skipper II
TypeRocket assisted, low-level, laser-guided bomb
Place of originUnited States
Service history
In service1985-1990s[1]
Used byUnited States Navy, United States Marine Corps
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)
Wingspan1.6 m (5 ft 3 in)
Warhead1000 lb (450 kg) Mk 83 bomb
Detonation
mechanism
Impact-fuse

EngineAerojet Mk 78 dual-thrust solid-fueled rocket
Operational
range
25 km (15.5 statute miles)
Maximum speed 1,100 km/h (680 mph)
Guidance
system
laser-guidance

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.

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Transcription

Design

The AGM-123 is composed out of a 1,000 lb (454 kg) Mark 83 low-drag general purpose bomb fitted with a Paveway guidance kit and one Aerojet Mk 78 solid-propellant rocket that fires upon launch. The rocket allows the AGM-123 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 was 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.[2]

Skipper missiles were also fired in Operation Desert Storm against Iraqi surface vessels by A-6s and U.S. Marine aircraft.[2]

Gallery

References

  1. ^ "Emerson Electric AGM-123 Skipper II". www.designation-systems.net.
  2. ^ a b "Islamic Republic News Agency" (in Persian). Archived from the original on 16 March 2012. Retrieved 20 March 2017.

External links

This page was last edited on 22 December 2023, at 12:04
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