The AGM-45 SHRIKE series weapon system is a passive air-to-ground missile whose mission is to home on and destroy or suppress radiating radar transmitters, directing both ground antiaircraft fire and surface-to-air missiles. The system consists of an AGM-45 guided missile, AERO-5A/B or LAU-118 launcher, and a launch aircraft configured with SHRIKE-unique avionics and a target identification acquisition system. The AGM-45 SHRIKE guided missile is composed of four major sections; guidance, warhead, control, and rocket motor. Along with the wing and fin assemblies, the sections make up the all-up-round missile. Several missile versions have been developed and produced to home on certain types of enemy radar transmitters. Each version consists of a guidance section specially developed and tuned to a specific frequency range unique to an individual threat radar. The AERO-5B-1 and LAU-118 series rail launchers are used to launch the SHRIKE missile. They provide the electrical and mechanical interface between the SHRIKE guided missile and the launch aircraft.
NOTS developed Shrike, the first successful antiradar missile, beginning in 1958 as a direct response to Fleet needs, and China Lake personnel took the missile to the carriers in Southeast Asia in the 1960s. During the Vietnam War, aircraft launched the first combat firing of the Shrike. Shrike was developed following many of the same principles that guided Sidewinder development: simplicity, reliability, maintainability, producibility, improvability. The AGM-45 was the first mass produced missile built specifically for the anti-radar mission, and more than 20,000 Shrikes were produced beginning in 1962. The Shrike's effectiveness was limitated by the requirement that the missile be pointed at the intended target radar during launch, and that the Shrike will lose its lock if the radar ceases to radiate. The Shrike is now being replaced by the much improved AGM-88 HARM.
|Manufacturer|| Texas Instruments,|
|Propulsion||Rocketdyne Mk 39 or Aerojet Mk 53 polybutadiene solid-fuel rocket|
|Speed||approx. Mach 2|
approx. 10 mi for AGM-45A|
up to 28.8 mi for AGM-45B with improved rocket motor
|Warhead||145 lbs conventional high-explosive/fragmentation|
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