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Cruise Missiles Β·Boeing

Missile AGM-86 ALCM

The AGM-86B ALCM is a US-developed nuclear-armed cruise missile introduced in 1982, designed for launch from B-52 bombers to strike strategic targets, featuring terrain-following guidance for low-altitude penetration. Key figures: range 2,400 km, top speed 890 km/h, warhead 132 kg, guidance Litton inertial navigation system with TERCOM updates, unit cost $1M, in service since 1982. In service with 1 country β€” United States.

Range
2,400km
Max speed
890km/h
Produced
1,715units
Avg unit price
$1million
Technical Specifications
WarheadW80-1 thermonuclear
Warhead weight132 kg (291 lb)
Nuclear yield150 kt
Diameter622 mm (24.5 in)
Span3,657 mm (144.0 in)
Length6,300 mm (248.0 in)
Weight1,458 kg (3,214 lb)
Range 2,400 km (1,491 mi)
Max. speed890 km/h (Mach 0.9)
AGM-86 ALCM scale diagram
AGM-86 ALCM β€” Cruise 1.75 m 6.30 m
Range
2,400 km
Speed
890 km/h
Weight
1.5 t
Warhead
132 kg
Nuclear Blast Simulator

See what a 150 kt strike from the AGM-86 ALCM would do to a real city: set ground zero anywhere on Earth and map the fireball, blast, thermal and radiation rings.

Operators
πŸ‡ΊπŸ‡Έ United States
Carried by

Description

The AGM-86 is an American subsonic air-launched cruise missile developed for the B-52G and B-52H. Its lineage begins with the ADM-20 Quail decoy of 1956, a small jet drone carrying jammers and radar reflectors to present false targets to Soviet defenses. As Quail's utility declined against improving Soviet air defenses, a replacement requirement was issued in January 1968 for the Subsonic Cruise Aircraft Decoy (SCAD), sized to fit the same rotary launcher as the AGM-69 SRAM and using a triangular fuselage cross-section to maximize launcher volume. The availability of small nuclear warheads led to the program being redesignated Subsonic Cruise Armed Decoy, and TERCOM guidance was added to correct inertial drift over long flight times. Development was approved in July 1970 under the designation ZAGM-86A. In June 1973 the decoy role was dropped entirely and the program became the Air Launched Cruise Missile. The first flight took place in March 1976, with the guidance system tested that September, and full-scale production was ordered in January 1977. A requirement for an Extended Range Version, combined with the cancellation of the B-1, ended the A-model. Under the Joint Cruise Missile Project the design adopted the AN/DPW-23 TERCOM set and Williams F107 turbofan of the Navy's sea-launched missile. The ERV flew in August 1979 and won a fly-off against the sea-launched design in March 1980.

All variants use the F107 turbofan and deploy folded wings, tail surfaces and engine inlet after launch. Launch is possible from high or low altitude. The AGM-86B navigates by TERCOM and carries a W80 thermonuclear warhead, a B61 derivative with selectable yields of 5 or 150 kilotons. The AGM-86C CALCM, first converted in June 1986, substitutes a blast/fragmentation warhead and replaces TERCOM with GPS coupled to the inertial navigation system. Block I CALCMs produced in 1996–1997 introduced a 1,360 kg blast-class payload and a multi-channel GPS receiver, subsequently retrofitted to earlier conversions. The AGM-86D carries a unitary penetrating warhead. A B-52H carries six missiles on each of two external pylons and eight internally on a rotary launcher.

Production of 1,715 missiles ran from fiscal year 1980 to October 1986. The AGM-86B reached operational status in December 1982 with the 416th Bombardment Wing at Griffiss AFB, New York, and was later fielded across the B-52G and B-52H fleet. Integration and flight testing were conducted with the B-1B but the missile was never operationally deployed on that aircraft. Between 1983 and 1993, 23 missiles were tested over northern Canada under the Canada-U.S. Test and Evaluation Program to simulate northern Soviet terrain and climate. The CALCM entered combat in January 1991 when seven B-52Gs from Barksdale AFB launched 35 missiles against Iraqi targets on sorties exceeding 14,000 miles and 35 hours. Thirteen were fired during Operation Desert Strike in September 1996, followed by use in Operation Desert Fox in 1998, Operation Allied Force in 1999, and Operation Iraqi Freedom in 2003, the latter marking the combat debut of the AGM-86D. The CALCM was retired on 20 November 2019.

Wikipedia (CC BY-SA) and other open sources. Last updated on 18 August 2026. Suggest a change

Frequently Asked Questions

What type of missile is the AGM-86 ALCM?
The AGM-86 ALCM is a cruise missile developed by the United States. It entered service in 1982.
What is the range of the AGM-86 ALCM?
The AGM-86 ALCM has a maximum range of approximately 2,400 km (1,491 miles). Effective range varies with launch platform, altitude, and flight profile.
How fast is the AGM-86 ALCM?
The AGM-86 ALCM reaches a maximum speed of 890 km/h (Mach 0.7).
What warhead does the AGM-86 ALCM carry?
The AGM-86 ALCM carries a w80-1 thermonuclear warhead weighing 132 kg.
How is the AGM-86 ALCM guided?
The AGM-86 ALCM uses litton inertial navigation system with TERCOM updates guidance.
Which countries use the AGM-86 ALCM?
The AGM-86 ALCM is in service with 1 country: United States.
How much does a AGM-86 ALCM cost?
The AGM-86 ALCM has an estimated unit cost of approximately $1 million. Actual prices vary by variant, quantity ordered, and support packages.
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Latest Data Updates
  1. AUG 182026 Updated Page refocused on the nuclear AGM-86B rather than the retired conventional AGM-86C/D
  2. JAN 242026 Updated Max speed added
  3. JAN 192026 Updated Number built, cost and 3 more fields added
  4. JAN 182026 Updated Sources and cross-references refreshed
  5. OCT 282023 Updated Specifications and description reviewed