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In 1963, the U.S. Department of Defense established a designation system for rockets and guided missiles jointly used by all the United States armed services. [1] It superseded the separate designation systems the Air Force and Navy had for designating US guided missiles and drones, but also a short-lived interim USAF system for guided missiles and rockets.
1963 United States Tri-Service rocket and guided missile designation system This page is a redirect . The following categories are used to track and monitor this redirect:
The Douglas GAM-87 Skybolt (AGM-48 under the 1963 Tri-service system) was a hypersonic air-launched ballistic missile (ALBM) developed by the United States during the late 1950s. The basic concept was to allow US strategic bombers to launch their weapons from well outside the range of Soviet defenses, as much as 1,000 miles (1,600 km) from ...
The Ford MGM-51 Shillelagh was an American anti-tank guided missile designed to be launched from a conventional gun (cannon). It was originally intended to be the medium-range portion of a short, medium, and long-range system for armored fighting vehicles in the 1960s and '70s to defeat future armor without an excessively large gun.
Unlike most other categories of aircraft, the introduction of the tri-service designation system in 1962 did not result in a wholesale redesignation of helicopters. While six types received new designations in the unified, "re-started" sequence, the original "H-" series of designations that started in 1948 was also continued, and no further ...
The AIM-68 was designed with a dual-thrust solid-propellant rocket and was capable of reaching speeds of Mach 4 over its 65-kilometre (40 mi) range. The prototypes were fitted with infrared guidance systems from GAR-2A/B (AIM-4C/D) Falcon missiles; the rocket motor from the AGM-12 Bullpup was used for propulsion.
The AGM-83 Bulldog was a missile produced by the United States.. The missile had its origins in the AGM-12 Bullpup.The Bullpup used a manual guidance system which required the launching aircraft to continue flying towards the target throughout the missile flight time, making it highly vulnerable to counterattack.
Development began in 1958, with the technical evaluation being completed in 1963. SUBROC reached Initial Operation Capability (IOC) aboard the attack submarine Permit in 1964. [ 5 ] [ 6 ] When SUBROC reached IOC, the US Navy's admiral in charge of weapons procurement stated that SUBROC was "…a more difficult technical problem than Polaris ."