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IOC: 1989
Total Production: 23,689
Unitary Cost: USD$129,000
Also Known As: AGM-65G2 Maverick
Origin: United States of America
Contractor/s: Raytheon
Description: The AGM-65 Maverick is a tactical air-to-surface missile designed to strike a wide range of surface fixed or moving targets. Maverick can be released from safe range minimizing exposure to the enemy's air defenses. AGM-65 is a modular design weapon allowing a different combination of warhead and guidance package. Due to this the Maverick evolved from TV-guided A model to current CCD-TV-guided H/K models. Maverick was used during operation Desert Storm, in 1991, achieving 85% of success rate. All Maverick models are powered by a single Thiokol TX-481 solid-propellant rocket motor.
The Maverick missile can be fired from virtually any western aircraft fighter. It has also been integrated on helicopters. For example AH-1W Super Cobra and New Zealand's Sea Sprite helicopters. Due to its characteristics Maverick is suitable even against small ships or boats. From 1972 to date more than 65,000 Maverick missiles have been produced for the United States and 27 international customers.
Maverick G is the follow-on Maverick D but the shaped-charge warhead has been replaced with a blast fragmentation warhead. The IR guidance system has been modified for optimized larger targets tracking.
Parent system is the AGM-65 Maverick
IOC: 1972
Total Production: 107,108
Total Cost: USD$8.3 billion
Other Family Members: AGM-65A Maverick, AGM-65B Maverick, AGM-65D Maverick, AGM-65E Maverick, AGM-65F Maverick, AGM-65H Maverick and AGM-65K Maverick
Transactions: There are 18 transactions involving 1,096 items for AGM-65 Maverick from 1994 to 2010 and 8 transactions involving 406 items for the AGM-65G Maverick view report
Applications:
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:: Reviews ::
:: Specifications ::
DimensionsDiameter: 300 millimeter (11.8 inch)
Length: 2.49 meter (98 inch)
Wingspan: 710 millimeter (28.0 inch)
PerformanceMax Range: 24,000 meter (13.0 nautical mile)
Min Range: 100 meter
WeightWarhead: 136 kilogram (300 pound)
Weight: 301 kilogram (664 pound)
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:: News ::
There are 13 news between 23 Jan 2003 and 12 Dec 2011
:: Operators ::
:: Image Gallery ::
There are 14 images added between 22 Nov 2006 and 7 Dec 2006
:: Notes & Resources ::
Last Updated: Saturday, February 2, 2013
(*) lead contractor
IOC: Initial Operating Capability
FOC: Full Operating Capability
CEP: Circular Error Probable
Comm: Commissioning Date
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Year (yr) Minutes (min) Second (sec)
Shaft-Horse-Power (shp)
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