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Measured figures
Length · source measurement 1
Single sourceLength · source measurement 2
Single sourceConfiguration
| Specification | Abu Mahdi (missile) | AGM-86 ALCM |
|---|---|---|
| Type | Cruise missile[source] | Air-to-ground strategic cruise missile[source] |
| Place of origin | Iran[source] | United States[source] |
| In service | 20 August 2020[source] | AGM-86B: 1982–present AGM-86C/D: retired[source] |
| Used by | Iran[source] |
Length · source measurement 3
Single source20 ft. 9 in. (6.3 m)[source]
AGM-86B
Single sourceAGM-86C Block 0 and AGM-86D
Single sourceAGM-86C Block 1
Single source1,458 kg (3,214 lb) (AGM-86B) 1,750 kg (3,860 lb) (AGM-86C Block 0 and AGM-86D) 1,950 kg (4,300 lb) (AGM-86C Block 1)[source]
Maximum; AGM-86B
Single sourceMaximum; AGM-86B Mach 0.73) AGM 86C: classified (nominal high subsonic
Single sourceAGM-86B: 550 mph (890 km/h, Mach 0.73) AGM 86C: classified (nominal high subsonic)[source]
Operational; AGM-86B: 1,500+ mi (2,400+ km) AGM-86C: classified (nominal
Single sourceOperational; Operational range
Single sourceAGM-86B: 1,500+ mi (2,400+ km) AGM-86C: classified (nominal 680 miles, 1,100 km)[source]
Williams International F107 -WR-101 turbofan engine thrust
Single sourceWilliams International F107 -WR-101 turbofan engine 600 lbf (2.7 kN) thrust[source]
AGM-86C Block 0
Single sourceAGM-86C Block 1
Single sourceclass advanced unitary penetrating warhead (AGM-86D)
Single source908kg (AGM-86C Block 0) 1362kg (AGM-86C Block 1) 1,200 lb (540 kg) class advanced unitary penetrating warhead (AGM-86D)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
United States Air Force[source] |
| Warhead | High Explosive[source] | W80 thermonuclear weapon (AGM-86B), 5 or 150 kilotons Conventional warhead (AGM-86C) AUP warhead (AGM-86D)[source] |
|---|
| Designed | — | 1974[source] |
|---|
| Manufacturer | — | Boeing Integrated Defense Systems[source] |
|---|
| Unit cost | — | $1 million (AGM-86B) additional $160,000 conversion cost for AGM-86C; additional $896,000 conversion cost for AGM-86D[source] |
|---|
| Produced | — | 1980[source] |
|---|
| No. built | — | 1,715 (AGM-86B) 239 (AGM-86C) 50 (AGM-86D)[source] |
|---|
| Variants | — | AGM-86B (1982), AGM-86C (1991), AGM-86D (2001)[source] |
|---|
| Guidance system | — | AGM-86B: Litton inertial navigation system element with TERCOM updates AGM 86C: Litton INS element integrated with multi-channel onboard GPS[source] |
|---|
| Launch platform | — | Boeing B-52H Stratofortress[source] |
|---|