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AGM-130 MISSILE

The first unit was operational in 1994.

Primary Function: Air-to-surface guided and powered bomb
Contractor: Boeing Co.
Thrust: Classified
Length: 12 feet, 10.5 inches (3.90 meters)
Launch Weight: 2,917 pounds (1,312.65 kilograms)
Diameter: 18 inches (45.72 centimeters)
Wingspan: 59 inches (149.86 centimeters)
Range: Classified
Ceiling: 30,000-plus feet (9,091 meters)
Speed: Classified
Guidance System: television/imaging infrared seeker man-in-the-loop; autonomous GPS/INS
Date Deployed: 1994
Unit Cost: Approximately $450,000 per weapon
Inventory: Classified.

AGM-65 MAVERICK

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
Inventory: Classified

AGM-86B/C MISSILES

General Characteristics
Primary Function: Air-to-ground strategic cruise missile
Contractor: Boeing Defense and Space Group.
Guidance Contractors: Litton Guidance and Control, and Interstate Electronics Corp. (AGM-86C model)
Power Plant: Williams Research Corp. F-107-WR-10 turbofan engine
Thrust: 600 pounds
Length: 20 feet, 9 inches (6.3 meters)
Weight: 3,150 pounds (1,429 kilograms)
Diameter: 24.5 inches (62.23 centimeters)
Wingspan: 12 feet (3.65 meters)
Range: AGM-86B: 1,500-plus miles; AGM-86C: 600 nautical miles (nominal); classified (specific)
Speed: AGM-86B, about 550 mph (Mach 0.73); AGM 86C, high subsonic (nominal), classified (specific)
Guidance System: AGM-86B, Litton inertial navigation element with terrain contour-matching updates; AGM 86C, Litton INS element integrated with multi-channel onboard GPS
Warheads: AGM-86B, Nuclear capable; AGM-86C; Block 0, 2,000 pound class, and Block I , 3,000 pound class
Unit Cost: AGM-86B, $1 million; AGM-86C, additional $160,000 conversion cost
Date Deployed: AGM-86B, December 1982; AGM-86C, January 1991
Inventory: AGM-86B, Active force, 1,142; ANG, 0; Reserve, 0.
AGM-86C, 239, Block 0, 41; Block I, 198

AGM-88 HARM

General Characteristics
Primary Function: Air-to-surface anti-radiation missile
Contractor: Raytheon Co.
Power Plant: Thiokol dual-thrust rocket motor
Thrust: Dual thrust
Length: 13 feet, 8 inches (4.14 meters)
Launch Weight: 800 pounds (360 kilograms)
Diameter: 10 inches (25.40 centimeters)
Wingspan: 3 feet, 8 inches (101.60 centimeters)
Range: 30 plus miles (48 plus kilometers)
Speed: Supersonic
Aircraft: Used aboard the F-16C
Guidance System: Proportional
Warheads: High explosive
Unit Cost: $200,000
Date Deployed: 1984

AIM-120 AMRAAM

General Characteristics
Primary Function: Air-to-air tactical missile
Contractor: Hughes Aircraft Co. and Raytheon Co.
Power Plant: High performance
Length: 143.9 inches (366 centimeters)
Launch Weight: 335 pounds (150.75 kilograms)
Diameter: 7 inches (17.78 centimeters)
Wingspan: 20.7 inches (52.58 centimeters)
Range: 20+ miles (17.38+ nautical miles)
Speed: Supersonic
Guidance System: Active radar terminal/inertial midcourse
Warhead: Blast fragmentation
Unit Cost: $386,000
Date Deployed: September 1991

AIM-7 SPARROW

General Characteristics
Primary Function: Air-to-air guided missile
Contractor: Raytheon Co.
Power Plant: Hercules MK-58 solid-propellant rocket motor
Thrust: Classified
Speed: Classified
Range: Classified
Length: 12 feet (3.64 meters)
Diameter: 8 inches (0.20 meters)
Wingspan: 3 feet, 4 inches (1 meter)
Warhead: Annular blast fragmentation warhead
Launch Weight: Approximately 500 pounds (225 kilograms)
Guidance System: Raytheon semiactive on either continuous wave or pulsed Doppler radar energy
Date Deployed: AIM-7F, 1976; AIM-7M, 1982
Unit Cost: Approximately $125,000
Inventory: Classified

AIM-9 SIDEWINDER

General Characteristics
Primary Function: Air-to-air missile
Contractor: Raytheon and Loral Martin
Power Plant: Hercules and Bermite Mk 36 Mod 11
Length: 9 feet, 5 inches (2.87 meters)
Diameter: 5 inches (0.13 meters)
Finspan: 2 feet, 3/4 inches (0.63 meters)
Warhead: Annular blast fragmentation warhead
Launch Weight: 190 pounds (85.5 kilograms)
Guidance System: Solid-state, infrared homing system
Introduction Date: 1956
Unit Cost: Approximately $84,000
Inventory: Classified

GBU-15

General Characteristics
Primary Function: Air-to-surface guided glide bomb
Contractor: Boeing North American for Legacy version; Raytheon Systems for Enhanced version
Length: 12 feet, 10.5 inches (3.91 meters)
Launch Weight: 2,500 pounds (1,125 kilograms)
Diameter: 18 inches (45.7 centimeters)
Wingspan: 4 feet, 11 inches (1.49 meters)
Range: 5-15 nautical miles
Ceiling: 30,000-plus feet (9,091 meters)
Speed: Classified
Guidance System: Television or imaging infrared seeker via man-in-the-loop link, autonomous GPS/INS
Warheads: MK-84 general purpose or BLU-109 penetrating bombs
Date Deployed: Legacy, 1983; Enhanced, 2001
Unit cost: TV: $242,500; IIR: $245,000
Inventory: Classified

JOINT DIRECT ATTACK MUNITIONS GBU 31/32

General Characteristics
Primary Function: Guided air-to-surface weapon
Contractor: Boeing Corp.
Length: (JDAM and warhead) GBU-31 (v) 1/B: 152.7 inches (387.9 centimeters); GBU-31 (v) 3/B: 148.6 inches (377.4 centimeters); GBU-32 (v) 1/B: 119.5 inches (303.5 centimeters)
Launch Weight: (JDAM and warhead) GBU-31 (v) 1/B: 2,036 pounds (925.4 kilograms); GBU-31 (v) 3/B: 2,115 pounds (961.4 kilograms); GBU-32 (v) 1/B: 1,013 pounds (460.5 kilograms)
Wingspan: GBU-31: 25 inches (63.5 centimeters); GBU-32: 19.6 ins. (49.8 centimeters)
Range: Up to 15 miles
Ceiling: 45,000-plus feet (13,677 meters)
Guidance System: GPS/INS
Unit cost: Approximately $21,000 per tailkit (FY 01 dollars)
Date Deployed: 1999
Inventory: The tailkit is in full-rate production. Projected inventory is 158,000; and 82,000 for the U.S. Navy

LANTIRN

General Characteristics
Primary function: Low altitude navigation and targeting infrared for night flying
Contractor: Lockheed Martin, Inc.
Length: Navigation pod, 78.2 inches (1.99 meters); targeting pod, 98.5 inches (2.51 meters)
Diameter: Navigation pod, 12 inches (.31 meters); targeting pod, 15 inches (.38 meters)
Weight: Navigation pod, 451.1 pounds (204.6 kilograms); targeting pod, 530 pounds (240.7 kilograms)
Aircraft: F-15E, F-16C/D
Sensors: Infrared and terrain following radar sensors are on the navigation pod. Infrared and laser designator and ranging sensors are on the targeting pod
Introduction Date: March 1987
Unit Cost: Navigation pod, $1.38 million; targeting pod, $3.2 million

LGM-30 MINUTEMAN III

General Characteristics
Primary Function: Intercontinental ballistic missile
Contractor: Boeing Co.
Power Plant: Three solid-propellant rocket motors; first stage - Thiokol; second stage - Aerojet-General; third stage - United Technologies Chemical Systems Division
Length: 59.9 feet (18 meters)
Weight: 79,432 pounds (32,158 kilograms)
Diameter: 5.5 feet (1.67 meters)
Range: 6,000-plus miles (5,218 nautical miles)
Speed: Approximately 15,000 mph (Mach 23 or 24,000 kph) at burnout
Ceiling: 700 miles (1,120 kilometers)
Thrust: First stage, 202,600 pounds
Load: Re-entry vehicle: Lockheed Martin Missiles and Space MK 12 or MK 12A
Guidance systems: Inertial system: Boeing North American; ground electronic/security system: Sylvania Electronics Systems and Boeing Co.
Unit cost: $7 million
Date deployed: June 1970, production cessation: December 1978
Inventory: Active force, 500; Reserve, 0; ANG, 0

LITENING II/ER/AT

General Characteristics
Primary function: Navigation and infrared/electro-optical targeting
Prime Contractor: Northrop Grumman Corporation teamed with Rafael Corporation
Length: 87 inches (2.20 meters)
Diameter: 16 inches (0.406 meters)
Weight: 440 pounds (200 kilograms)
Aircraft: A-10, B-52H, F-15E, F-16 Block 25/30/32/40/42/50/52
Sensors: Infrared detector, CCD-TV camera, laser rangefinder and laser designator
Date Deployed: February 2000
Unit Cost: $1.4 million