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MISSILES Missile Deployment National Missile Forces Missile Types
AGM-88 HARM
 
AGM-88 HARM
Country: USA
Type: ARM
Introduction: 1984

The AGM-88 High-speed Anti-Radiation Missile (HARM) is an air-to-surface tactical missile designed to home in on electronic transmissions associated with surface-to-air missile radar systems. The missile was originally developed by Texas Instruments as a replacement for the AGM-45 Shrike and AGM-78 Standard ARM system. The AGM-88 is in service with the US Navy and Air Force.

The AGM-88 can detect, attack and destroy a radar antenna or transmitter with minimal aircrew input. The proportional guidance system that homes in on enemy radar emissions has a fixed antenna and seeker head in the nose of the missile. A smokeless, solid-propellant, dual-thrust rocket motor propels the missile at speeds up to Mach 2. HARM, a Navy-led program, was integrated onto the A-6E, A-7 and F/A-18 initially and later onto the EA-6B. The Air Force introduced HARM onboard the F-4G Wild Weasel and later on specialized F-16 aircraft equipped with the HARM Targeting System.

The HARM missile was approved for full production in March 1983 and deployed in late 1985. The newest upgrade is the AGM-88E Advanced Anti Radiation Guided Missile (AARGM). The AARGM will feature the latest software and enhanced capabilities, intended to counter radar shutdown.


TECHNICAL SPECIFICATIONS

General Information
Developed by USA
Deployed by Germany, Greece, Italy, South Korea, Spain, Turkey, USA
Development Year 1972
Deployment Year 1984
Platform (US Navy) EA-6B, F/A-18, A-7E, A-6E, F-14 (US Air Force) F-4G Wild Weasel, F-16C/D
Number manufactured 21,012 (USN:9,742, USAF:9,865, export:1,405)
Contractor US Naval Air Systems Command, Texas Instruments (system integrator), Raytheon Co., Raytheon Systems Co., Defense Systems Div.

Dimensions and Performance
Length 4.14m
Body Diameter 25.4cm
Wing/Fin span 1.13m
Launch Weight 363kg
Range 125km
Speed Mach 2+

Components
Propulsion solid propellant
Engine Thiokol and Hercules T/YSR-113-TC-1 dual-thrust low smoke solid rocket motor
Warhead 66.4kg HE fragmentation effect
Guidance strapdown inertial, anti-radar homing