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AGM-86 ALCM vs Kh-55

AGM-86 ALCM vs Kh-55 at a glance — range 2,400 vs 2,500 km, speed 890 vs 750 km/h, warhead 132 vs 410 kg, launch weight 1,458 vs 1,500 kg.

Specifications
AGM-86 ALCM Kh-55
Origin 🇺🇸 United States 🇷🇺 Russia🇷🇺 Ex-USSR
Category Cruise Cruise
Type Air-launched cruise missile Cruise missile
Manufacturer Boeing Raduga OKB
Service year 1982 1983
Number produced 1,715 units -- units
Estimated unit price $1 million NA
Range 2,400.0 km 2,500.0 km
Maximum speed 890 km/h 750 km/h
Weight 1,458 kg 1,500 kg
Warhead 132.0 kg 410.0 kg
Length 6.30 m 6.04 m
Diameter 622 mm 510 mm
Guidance Litton inertial navigation system with TERCOM updates Inertial, Doppler radar, terrain map updates
Warhead type W80-1 thermonuclear Nuclear
Scale Comparison
AGM-86 ALCM 6.30 m KH-55 6.04 m 1.75 m
Performance Radar Chart

Detailed Comparison

The AGM-86 and Kh-55 originated as Cold War strategic air-launched cruise missiles designed to penetrate integrated air defense systems via low-altitude, subsonic flight profiles. Both platforms provided standoff capabilities for heavy bombers—the Boeing B-52H for the American missile, and the Tupolev Tu-95MS and Tu-160 for the Soviet weapon. Over their lifespans, both architectures transitioned from strictly nuclear deterrence to conventional strike operations on different timelines.

Development and Design

Boeing developed the AGM-86 in the late 1970s, producing over 1,700 units primarily as the nuclear-armed AGM-86B. Subsequent arms reduction treaties drove the conversion of hundreds of these airframes into the conventional AGM-86C/D Conventional Air-Launched Cruise Missile (CALCM). Raduga OKB designed the Kh-55 concurrently. The Russian missile utilizes a drop-down turbofan engine, compared to the AGM-86's integrated fuselage design. The Kh-55 spawned several variants, including the conventional Kh-555 and the export variant Kh-65SE. Authorized export failed, but illicit transfers of Kh-55s to Iran and China occurred in 2001, providing the basis for Iran's Soumar missile family.

Performance and Capabilities

The nuclear Kh-55 achieves a 2,500 km range, outdistancing the conventional AGM-86C's 1,110 km reach. Both operate at high-subsonic speeds (AGM-86 at 900 km/h, Kh-55 at 750 km/h). The CALCM carries a 680 kg blast-fragmentation or penetrating warhead (AFX-760), optimized for hardened targets. The baseline Kh-55 carries a 200-kiloton nuclear payload weighing 410 kg. Both missiles rely on low-altitude flight profiles (under 150 meters) to mask their radar cross-sections from ground-based interceptors. Neither airframe is stealthy, leaving them susceptible to modern look-down/shoot-down fighter radars.

Guidance and Technology

Initially reliant on Inertial Navigation Systems (INS) and Terrain Contour Matching (TERCOM), the AGM-86C integrated multi-channel GPS in the late 1980s, achieving circular error probable (CEP) metrics under 10 meters. The Kh-55 utilizes a similar Doppler radar and terrain map update system. Post-Soviet modernization programs retrofitted GLONASS receivers onto the Kh-55 airframe. The Russian platform's reliance on older terrain-mapping algorithms historically resulted in higher failure rates over flat terrain compared to the GPS-augmented CALCM.

Deployment and Combat Record

The USAF launched the AGM-86C in multiple conflicts. B-52Hs fired 35 CALCMs during Operation Desert Storm in 1991, with subsequent use in Desert Strike (1996), Desert Fox (1998), and Allied Force (1999). The baseline Kh-55 never saw nuclear combat. However, the Russian Aerospace Forces launched conventional Kh-555s during the Syrian Civil War. During the 2022-2024 invasion of Ukraine, Russia deployed aging Kh-55s equipped with inert dummy warheads to act as decoys, intentionally drawing fire from Ukrainian Patriot and NASAMS batteries to deplete interceptor stockpiles.

Conclusion

The AGM-86 possesses the edge in conventional, precision-strike scenarios. Its early integration of GPS and repeated combat testing during the 1990s refined its targeting software, making the CALCM a reliable anti-infrastructure weapon until its retirement in favor of the JASSM. The Kh-55 retains utility primarily as an attritional decoy. Its lack of a purpose-built conventional variant until late in its service life, combined with a higher rate of subsystem failure observed in Ukraine, relegates the Kh-55 to a secondary asset compared to modern Russian munitions like the Kh-101.

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Frequently Asked Questions

Which has longer range, the AGM-86 ALCM or Kh-55?
The Kh-55 has a longer range at 2,500 km compared to the AGM-86 ALCM's 2,400 km.
Which is faster, the AGM-86 ALCM or Kh-55?
The AGM-86 ALCM is faster with a maximum speed of 890 km/h compared to the Kh-55's 750 km/h.
Which has a larger warhead, the AGM-86 ALCM or Kh-55?
The Kh-55 carries a larger warhead at 410 kg compared to the AGM-86 ALCM's 132 kg.
Which is heavier, the AGM-86 ALCM or Kh-55?
The Kh-55 is heavier at 1,500 kg compared to the AGM-86 ALCM's 1,458 kg.
Which is longer, the AGM-86 ALCM or Kh-55?
The AGM-86 ALCM is longer at 6.30 meters compared to the Kh-55's 6.04 meters.
What guidance systems do the AGM-86 ALCM and Kh-55 use?
The AGM-86 ALCM uses Litton inertial navigation system with TERCOM updates guidance while the Kh-55 uses Inertial, Doppler radar, terrain map updates guidance.
Which entered service first, the AGM-86 ALCM or Kh-55?
The AGM-86 ALCM entered service first in 1982, 1 years before the Kh-55 which entered service in 1983.