AGM-86
Initial Operational Capability (IOC) : 1982
Total Production : 1,739
Total Cost : USD $1.7 billion
The AGM-86 is an air launched subsonic cruise missile developed to increase effectiveness of B-52 bombers during the Cold War. It entered active service in the US Air Force in 1982 and 1,739 AGM-86s were produced through September 1986. The conventional AGM-86 missile was used in combat for the first time in Operation Desert Storm in 1991. Afterward it was tested in Operation Desert Fox, Desert Strike, Allied Force, Enduring Freedom and Operation Iraqi Freedom. The AGM-86 is the longest range conventional armed missile in the US Air Force inventory and provides the B-52 with the capability to accurately strike nearly any target in the world, without the support of bases located outside the continental United States.
Model | Status | Year | Produced |
---|---|---|---|
AGM-86B ALCM | Active | 1982 | 1,739 |
AGM-86C CALCM | Active | 1988 | ? |
AGM-86D CALCM | Active | 2001 | ? |
AGM-86B ALCM
Group : Cruise Missiles
Status : Active
Also Known As : Air Launched Cruise Missile
Origin : United States of America
Contractor : Boeing
Initial Operational Capability (IOC) : 1982
Total Production : 1,739
Unitary Cost : USD $1.0 million
The AGM-86B ALCM (Air Launched Conventional Missile) is armed with a nuclear warhead and can be carried and launched internally and externally from the B-52H bomber. Its long range allows the B-52H to operate out of the enemy air defenses while AGM-86B's cruise flight profile makes itself survivable against the air defenses. The navigation system consists of a terrain-correlation system which provides location updates in flight. The US Air Force plans to convert part of existing nuclear-armed AGM-86Bs to conventionally-armed AGM-86C/D configurations.
Operators
Country | Status | State | Notes |
---|---|---|---|
![]() | Active | 1,142/1,739 |
Specifications
Notes | ||
---|---|---|
Dimensions | ||
Diameter | 620 millimeter | |
Length | 6.3 meter | |
Wingspan | 3.7 meter | |
Mass | ||
Thrust | 600 pound | |
Weight | 1,429 kilogram | |
Performance | ||
Max Range | 2,450 kilometer | |
Speed | ||
Top Speed | 242 mps | |
Yield | ||
Yield | 150 kiloton |
Gear
Warheads | ||
---|---|---|
W80 | 1 |
AGM-86C CALCM
Group : Cruise Missiles
Status : Active
Also Known As : Conventional Air Launched Cruise Missile
Origin : United States of America
Contractor : Boeing
Initial Operational Capability (IOC) : 1988
Total Production : ?
Unitary Cost : USD $1.2 million
The AGM-86C CALCM (Conventional Air Launched Cruise Missile) employs a GPS coupled with an Inertial Navigation System (INS) to achieve its mission. This navigation system allows the missile to guide itself with pinpoint accuracy. A single B-52H is able to carry and deliver up to 20 CALCMs. CALCMs are a modification of existing ALCMs instead of new production missiles. They have been procured under 3 batches known as Block 0, Block 1, and Block 1A and featuring different improvements, specially accuracy and warhead. The AGM-86C is provided with a conventional blast/fragmentation warhead. The US Air Force plans to convert further ALCMs to CALCM configuration.
Operators
Country | Status | State | Notes |
---|---|---|---|
![]() | Active | 478/468 |
Specifications
Notes | ||
---|---|---|
Dimensions | ||
Diameter | 620 millimeter | |
Length | 6.3 meter | |
Wingspan | 3.7 meter | |
Mass | ||
Thrust | 600 pound | |
Warhead | 907 kilogram | |
Weight | 1,475 kilogram | |
Performance | ||
Max Range | 1,100 kilometer | |
Speed | ||
Top Speed | 223 mps |
AGM-86D CALCM
Group : Cruise Missiles
Status : Active
Also Known As : Conventional Air Launched Cruise Missile
Origin : United States of America
Contractor : Boeing
Initial Operational Capability (IOC) : 2001
Total Production : ?
Unitary Cost : USD $1.2 million
The AGM-86D CALCM has been develop to meet the US Air Force requirements against hardened and buried targets. The D model features a Lockheed-Martin AUP penetration warhead capable of piercing up to 12 feet of concrete.
Operators
Country | Status | State | Notes |
---|---|---|---|
![]() | Active | 50/195 |
Specifications
Notes | ||
---|---|---|
Dimensions | ||
Diameter | 620 millimeter | |
Length | 6.3 meter | |
Wingspan | 3.7 meter | |
Mass | ||
Thrust | 600 pound | |
Warhead | 907 kilogram | |
Weight | 1,475 kilogram | |
Performance | ||
Max Range | 1,100 kilometer | |
Piercing in Concrete | 12 foot | |
Speed | ||
Top Speed | 223 mps |
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Photo Gallery
Notes
State Latest Known holdings/Original Procurement
Com - Date of Commissioning
Decom - Date of Decommissioning
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