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General Characteristics Primary Function: Air-to-surface guided missile Contractors: Raytheon Systems Co. Power Plant: Thiokol TX-481 solid-propellant rocket motor Launch Weight: AGM-65B/H, 462 pounds (207.90 kilograms); AGM-65D, 485 pounds (218.25 kilograms); AGM-65E, 777 pounds (353.2 kilograms); AGM-65F, 804 pounds (365.5 kilograms); AGM-65G, 670 pounds (301.50 kilograms); AGM-65K, 793 pounds (360.45 kilograms) Diameter: 1 foot (30.48 centimeters) Wingspan: 2 feet, 4 inches (71.12 centimeters) Range: Classified Speed: Classified Aircraft: Used aboard A-10, F-15E and F-16 Guidance System: AGM-65B/H/K, electro-optical television; AGM-65D/F/G, imaging infrared; AGM-65E, laser guided Warheads: AGM-65B/D/H, 125 pounds (56.25 kilograms), cone shaped; AGM-65E/F/G/K, 300 pounds (135 kilograms) delayed-fuse penetrator, heavyweight Unit Cost: $17,000 to $110,000 depending on the Maverick variant Date Deployed: August 1972 |
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