and the re-entry vehicles plunging into the Atlantic Ocean, 1981 The launch from the submarine occurs below the sea surface. The missiles are ejected from their tubes by igniting an explosive charge in a separate container. The energy from the blast is directed to a water tank, where the water is flash-vaporized to steam. The subsequent pressure spike is strong enough to eject the missile out of the tube and give it enough momentum to reach and clear the surface of the water. The missile is pressurized with
nitrogen to prevent the intrusion of water into any internal spaces, which could damage the missile or add weight, destabilizing the missile. Should the missile fail to breach the surface of the water, there are several safety mechanisms that can either deactivate the missile before launch or guide the missile through an additional phase of launch. Inertial motion sensors are activated upon launch, and when the sensors detect downward acceleration after being blown out of the water, the first-stage motor ignites. The
aerospike, a telescoping outward extension that halves aerodynamic drag, is then deployed, and the boost phase begins. When the third-stage motor fires, within two minutes of launch, the missile is traveling faster than 20,000 ft/s (6,000 m/s, 13,600 mph, 21,600 km/h, or Mach 18). Minutes after launch, the missile is outside the atmosphere and on a
sub-orbital trajectory. The guidance system for the missile was developed by the
Charles Stark Draper Laboratory and is maintained by a joint Draper/General Dynamics Mission Systems facility. It is an
inertial navigation system with an additional
star-sighting system (this combination is known as
astro-inertial guidance), which is used to correct small position and velocity errors that result from launch condition uncertainties due to errors in the submarine navigation system and errors that may have accumulated in the guidance system during the flight due to imperfect instrument calibration. GPS has been used on some test flights but is assumed not to be available for a real mission. The fire control system was designed and continues to be maintained by General Dynamics Mission Systems. Once the star-sighting has been completed, the "bus" section of the missile maneuvers to achieve the various velocity vectors that will send the deployed multiple independent reentry vehicles to their individual targets. The downrange and crossrange dispersion of the targets remains classified. The Trident was built in two variants: the I (C4) UGM-96A and II (D5) UGM-133A; however, these two missiles have little in common. While the C4, formerly known as EXPO (extended range poseidon), is just an improved version of the Poseidon C-3 missile, the Trident II D-5 has a completely new design (although with some technologies adopted from the C-4). The C4 and D5 designations put the missiles within the "family" that started in 1960 with
Polaris (A1, A2 and A3) and continued with the 1971
Poseidon (C3). Both Trident versions are three-stage, solid-propellant, inertially guided missiles, and both guidance systems use a star sighting to improve overall weapons system accuracy.
Trident I (C4) UGM-96A , Florida The first eight
Ohio-class submarines were built with the Trident I missiles.
Trident II (D5) UGM-133A ballistic missile submarine. The second variant of the Trident is more sophisticated and can carry a heavier payload. It is accurate enough to be a
first strike,
counterforce, or
second strike weapon. All three stages of the Trident II are made of
graphite epoxy, making the missile much lighter. The Trident II was the original missile on the British
Vanguard-class and American
Ohio-class SSBNs from
Tennessee on. The D5 missile is currently carried by fourteen
Ohio-class and four
Vanguard-class SSBNs. There have been 191 successful test flights of the D5 missile since design completion in 1989, the most recent being from in September 2023. There have been fewer than 10 test flights that were failures, the most recent being from in January 2024. This is the second failure in a row for the Royal Navy after a launch from , one of Britain's four nuclear-armed submarines, off the coast of Florida in June 2016. The
Royal Navy operates their missiles from a shared pool, together with the Atlantic squadron of the
U.S. Navy Ohio-class SSBNs at
King's Bay, Georgia. The pool is 'co-mingled' and missiles are selected at random for loading on to either nation's submarines.
D5LE (D5 Life Extension Program) In 2002, the United States Navy announced plans to extend the life of the submarines and the D5 missiles to the year 2040. This requires a D5 life extension program (D5LEP), which is currently underway. The main aim is to replace obsolete components at minimal cost by using commercial off the shelf (COTS) hardware; all the while maintaining the demonstrated performance of the existing Trident II missiles. In 2007,
Lockheed Martin was awarded a total of $848 million in contracts to perform this and related work, which also includes upgrading the missiles' reentry systems. On the same day, Draper Labs was awarded $318 million for upgrade of the guidance system. The first flight test of a D-5 LE subsystem, the MK 6 Mod 1 guidance system, in
demonstration and shakedown operation (DASO)-23, took place on on 22 February 2012. This was almost exactly 22 years after the first Trident II missile was launched from
Tennessee in February 1990.
D5LE2 (D5 Life Extension Program 2) US Navy Vice Admiral Johnny Wolfe, in charge of overall submarine weapons systems procurement, indicated in 2020 that he had initiated trade studies to apply lessons from the D5LE program to extend the Trident II's lifespan to 2084. Wolfe said he expected the first D5LE2 missiles to be deployed aboard the ninth
Columbia-class submarine by FY 2039. ==Conventional Trident==