Generated by DeepSeek V3.2| AGM-129 ACM | |
|---|---|
| Name | AGM-129 ACM |
| Caption | An AGM-129A Advanced Cruise Missile |
| Type | Stealth air-launched cruise missile |
| Origin | United States |
| Used by | United States Air Force |
| Designer | General Dynamics |
| Manufacturer | General Dynamics |
| Unit cost | $6.6 million (1999) |
| Production date | 1985–1993 |
| Service | 1990–2012 |
| Engine | Williams International F112-WR-100 turbofan |
| Weight | 3,500 lb (1,590 kg) |
| Length | 20 ft 10 in (6.35 m) |
| Wingspan | 10 ft 2 in (3.10 m) |
| Speed | Subsonic |
| Range | 1,500 mi (2,400 km) |
| Guidance | Inertial navigation system with Terrain Contour Matching (TERCOM) and GPS updates |
| Warhead | W80-1 thermonuclear warhead |
| Launch platform | B-52 Stratofortress |
AGM-129 ACM was a stealth air-launched cruise missile developed for the United States Air Force to deliver a nuclear weapon against hardened strategic targets. Designed to penetrate sophisticated Soviet Air Defence Forces networks, it represented a significant technological leap over its predecessor, the AGM-86 ALCM. The missile entered service with Strategic Air Command in 1990, providing a key component of the U.S. strategic nuclear triad until its retirement in 2012.
The development of the AGM-129 Advanced Cruise Missile was initiated in the early 1980s by General Dynamics under a contract from the United States Department of Defense. The primary design objective was to create a low-observable weapon capable of evading detection and interception by advanced Soviet surface-to-air missile systems like the S-300. Engineers incorporated extensive stealth technology, including a faceted airframe, radar-absorbent materials, and an infrared signature-suppressing engine inlet. The propulsion system featured a highly efficient Williams International turbofan engine mounted above the fuselage to shield its exhaust from ground-based sensors. Guidance relied on a sophisticated blend of an inertial navigation system, Terrain Contour Matching (TERCOM), and later integration with the Global Positioning System for exceptional accuracy.
The AGM-129 ACM achieved initial operational capability in 1990, entering the inventory of Strategic Air Command and being deployed aboard the B-52 Stratofortress bombers of units like the 2nd Bomb Wing at Barksdale Air Force Base. Its introduction coincided with the final years of the Cold War and the subsequent signing of arms control treaties such as START I. Throughout the 1990s, the missile remained a cornerstone of U.S. strategic deterrence, though its operational life was marred by significant maintenance and reliability challenges. Following the September 11 attacks and a shift in national security priorities, the George W. Bush administration ordered the retirement of the entire AGM-129 fleet as part of broader nuclear force reductions, with the last missile withdrawn from service in 2012.
The missile was 20 feet 10 inches in length with a wingspan of 10 feet 2 inches, and it weighed approximately 3,500 pounds. Its airframe utilized composite materials and a unique shape to minimize its radar cross-section. Propulsion was provided by a single Williams International F112-WR-100 turbofan engine, granting a subsonic cruising speed and an operational range exceeding 1,500 miles. The guidance suite combined an inertial navigation system with Terrain Contour Matching and GPS satellite updates for precise navigation. It was armed exclusively with a single W80-1 thermonuclear warhead, a variable-yield device derived from the B61 nuclear bomb family.
Only one major production variant, the AGM-129A, was ever fielded. A proposed conventional (non-nuclear) version, sometimes referenced as the AGM-129B, was studied but never advanced beyond the concept stage due to cost and the emergence of newer weapons like the AGM-158 JASSM. The basic AGM-129A design itself saw incremental updates throughout its service life, primarily involving software improvements to its guidance system and integration of newer GPS capabilities to maintain targeting precision.
Deployed exclusively aboard the B-52 Stratofortress, each aircraft could carry up to twelve missiles on underwing pylons and an internal Common Strategic Rotary Launcher. The AGM-129's primary strategic role was to serve as a survivable, penetrating counterforce weapon, targeting heavily defended installations such as ICBM silos, command centers like the Kremlin, and key military-industrial sites deep within the territory of the Soviet Union. Its stealth characteristics were intended to complicate enemy air defense planning and ensure the credibility of the U.S. strategic deterrent. Following the Cold War, its role evolved under policies outlined in documents like the Nuclear Posture Review, ultimately being retired in favor of maintaining and modernizing other legs of the nuclear triad, including the newer AGM-86 and the future Long Range Standoff Weapon.
Category:Air-to-surface missiles of the United States Category:Nuclear cruise missiles Category:Cold War missiles of the United States