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BCruise & anti-ship missiles
Anti-ship cruise missile Surface-to-surface missile Submarine-launched cruise missile
At a glance
AGM-86 ALCMlarger figure on 2 of 2
Atmacalarger figure on 0 of 2
Counts only measures both sources give with the same scope. A larger figure is not a better system.
Measured figures
Length · source measurement 1
Single sourceLength · source measurement 2
Single sourceConfiguration
| Specification | AGM-86 ALCM | Atmaca |
|---|---|---|
| Type | Air-to-ground strategic cruise missile[source] | Anti-ship cruise missile Surface-to-surface missile Submarine-launched cruise missile[source] |
| Place of origin | United States[source] | Turkey[source] |
| In service | AGM-86B: 1982–present AGM-86C/D: retired[source] | 2020[source] |
| Used by | United States Air Force[source] | See Users |
Length · source measurement 3
Single source20 ft. 9 in. (6.3 m)[source]
Length
Single source4,800 - 5,200 mm[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]
Army version
Single sourceNavy version
Single sourceNavy version: 750 kg Army version: 890 kg
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]
Effective; Land version
Single sourceEffective; Navy version
Single sourceWilliams 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]
Army version
Single sourceNavy version
Single sourceBars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Designed | 1974[source] | 2009-2018[source] |
|---|
| Manufacturer | Boeing Integrated Defense Systems[source] | Roketsan[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] | 2018[source] |
|---|
| No. built | 1,715 (AGM-86B) 239 (AGM-86C) 50 (AGM-86D)[source] | Unknown[source] |
|---|
| Variants | AGM-86B (1982), AGM-86C (1991), AGM-86D (2001)[source] | See Variants[source] |
|---|
| Warhead | W80 thermonuclear weapon (AGM-86B), 5 or 150 kilotons Conventional warhead (AGM-86C) AUP warhead (AGM-86D)[source] | High-explosive penetrating warhead[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] | INS/GPS+RA+DL[source] |
|---|
| Launch platform | Boeing B-52H Stratofortress[source] | Frigates Corvettes Submarine Patrol boats Coastal defense batteries Unmanned surface vehicle[source] |
|---|
| Designer | — | Roketsan[source] |
|---|
| Engine | — | Kale KTJ-3200 Kale KTJ-3700 Microturbo TRI-40 (First versions)[source] |
|---|
| Propellant | — | Aviation-grade kerosene[source] |
|---|
Navy version: 250 km Land version: 400 km[source]
Navy version: 220 kg Army version: 250 kg[source]