AGM-88 HARM | |
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Type | Air-to-surface anti-radiation missile |
Place of origin | United States |
Service history | |
In service | 1985–present |
Used by | See list of operators |
Wars | |
Production history | |
Designer | Texas Instruments, Alliant Techsystems (ATK) |
Designed | 1983 |
Manufacturer | Texas Instruments, then Raytheon Missiles & Defense (AGM-88A/B/C/D/F) Alliant Techsystems, then Orbital ATK, then Northrop Grumman (AGM-88E/G) |
Unit cost | US$284,000 US$870,000 for AGM-88E AARGM[1] |
Produced | 1983–present |
Specifications | |
Mass |
|
Length |
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Diameter |
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Wingspan | 3 ft 8 in (1.13 m) |
Warhead | WAU-7/B blast-fragmentation warhead |
Warhead weight | 150 lb (68 kg) |
Engine | Thiokol SR113-TC-1 dual-thrust rocket engine |
Propellant | Two stage, solid propellant |
Operational range |
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Maximum speed | Mach 2.9 (987 m/s; 3238 ft/s) |
Guidance system | Passive radar homing with home-on-jam, additional GPS/INS and millimeter-wave active radar homing in the E and G variants |
Launch platform | F-4G, EA-6B, F-15E, F-16, F/A-18A/B/C/D, F/A-18/E/F, EA-18G, Tornado IDS/ECR, Eurofighter Typhoon, F-35, MiG-29, Su-27 |
References | Janes[2][3] |
The AGM-88 HARM (High-speed Anti-Radiation Missile) is a tactical, air-to-surface anti-radiation missile designed to home in on electronic transmissions coming from surface-to-air radar systems. It was originally developed by Texas Instruments as a replacement for the AGM-45 Shrike and AGM-78 Standard ARM system. Production was later taken over by Raytheon Corporation when it purchased the defense production business of Texas Instruments.