AGM-129 ACM - Design, Test and Initial Production

Design, Test and Initial Production

In 1983 General Dynamics Convair Division (GD/C) was awarded a development contract for the AGM-129A. The AGM-129A incorporated body shaping and forward swept wings to reduce the missile's radar cross section. The engine air intake was flush mounted on the bottom of the missile to further improve radar cross section. The jet engine exhaust was shielded by the tail and cooled by a diffuser to reduce the infra-red signature of the missile. To reduce electronic emissions from the missile, the radar used in the AGM-86B was replaced with a combination of inertial navigation and terrain contour matching TERCOM enhanced with highly accurate speed updates provided by a laser Doppler velocimeter.

These changes made the AGM-129A more difficult to detect and allowed the missile to be flown at higher altitude. The newer Williams International F112-WR-100 turbofan engine increased range by about 50%. The newer guidance system, increased accuracy to a quoted figure of between 30 m (100 ft) and 90 m (300 ft).

The AGM-129A like the AGM-86B is armed with a W80-1 variable yield nuclear warhead.

The first test missile flew in July 1985 and the first production missiles were delivered to the US Air Force in 1987. The development program experienced some hardware quality control problems and testing mishaps. The flight test program took place during a period of high tension between the machinist's union and GDC management, with a 3 1/2 week long strike occurring in 1987. US Congressman Les Aspin called the ACM a procurement disaster with the worst problems of any of the eight strategic weapons programs his committee had reviewed. The US Congress zeroed out funding for the ACM program in 1989. Manufacturing quality problems led the US Air Force to stop missile deliveries in 1989 and 1991. McDonnell Douglas was invited to qualify as a second source for missile production. In early 1989, the United States requested and received permission to test the AGM-129A in Canada.

Plans called for producing enough missiles to replace the approximately 1,461 AGM-86B's at a rate of 200 missiles per year after full-rate production was achieved in 1993. In January 1992, the end of the Cold War led US President George H.W. Bush to announce a major cutback in total ACM procurement. The President determined that only 640 missiles were needed. The ACM program was later reduced still further to 460 missiles. In August 1992 General Dynamics sold its missile business to Hughes Aircraft Corporation. Five years later in 1997, Hughes Aircraft Corporation sold its aerospace and defense business to the final production contractor Raytheon.

The US Air Force pushed for production of a AGM-129B variant for targets for which the AGM-129A was considered ineffective. The US Air Force submitted this requirement in 1985 and proposed to modify 120 missiles into the AGM-129B variant. In 1991 the US Congress denied the request and the US Air Force was forced to terminate the program. In 1992, the US Air Force was directed by the US Department of Defense to restart the program, an effort which was opposed by the General Accounting Office of the US Congress. Confusion exists as to precisely how this weapon is different from the original. The Department of Defense document DoD 4120.15-L "Model Designation of Military Aerospace Vehicles" states that the AGM-129B was a AGM-129A "modified with structural and software changes and an alternate nuclear warhead for accomplishing a classified cruise missile mission." However, Ozu states the AGM-129B was intended to be a non-nuclear version of the ACM, much as the nuclear AGM-86B led to the conventional AGM-86C.