| Mk 41 vertical launching system | |
| Origin: | United States |
| Type: | Missile launching system |
| Is Ranged: | yes |
| Service: | 1986–present |
| Used By: | United States Navy Royal Navy |
| Wars: | Cold War Tanker War Gulf War Kosovo War War on Terror Red Sea crisis |
| Design Date: | 1970s |
| Manufacturer: | Martin Marietta Lockheed Martin |
| Variants: | Mk 57 Mk 70 Mod 1 |
The Mark 41 vertical launching system (Mk 41 VLS) is a shipborne missile canister launching system which provides a rapid-fire launch capability against hostile threats.[1] The vertical launching system (VLS) concept was derived from work on the Aegis Combat System.[2]
Refinement of the initial concept of Aegis system in the 1960s continued through the 1960s and 1970s, and the Mk 41 was conceived in 1976.[2] Originally, the system was only intended to fire the RIM-66 Standard missile, but the height of the Mk 41 was increased to accommodate the larger Tomahawk missile.[2] The prototype for the launcher was tested and evaluated on board . The first operational launcher was installed aboard .[2]
On 12 October 2016, was targeted by missiles fired from Yemeni territory while operating in the Bab-el-Mandeb strait.[3] Mason was not hit by the two missiles, which were fired from near the city of Al Hudaydah. While the Navy is not certain whether the first incoming missile was intercepted or it just fell into the sea, officials claim Mason successfully intercepted the second missile at a distance of about,[4] marking the first time in history a warship destroyed an inbound anti-ship missile with a SAM in actual self-defense and the first time the Mk41 VLS did so.
The Mk 41 is capable of firing the following missiles:[5] [2] [6] [7]
The missiles are pre-loaded into "canisters", which are then loaded into the individual "cells" of the launcher. The ESSM is loaded in a quad-pack with 4 missiles in one Mk 25 canister, older types of 8 cell modules are not able to use ESSM. Lockheed Martin has developed the Host Extensible Launching System (ExLS), an adapter for Mark 41 and Mark 57 vertical launching systems that was designed to allow for easier integration of new or existing weapon systems such as Nulka, RAM Block 2, CAMM and CAMM-ER, and the Joint Air to Ground Missile (JAGM) in a quad-packed configuration.[8] [9] [10] Some munitions under development such as CAMM-MR are planned to be dual-packed (likely with ExLS) with two missiles sharing a single canister enabling larger and longer range munitions to be carried in greater quantity.[11]
Launcher cells are fitted to ships in 8 cell modules (2 rows of 4) that share a common uptake hatch (exhaust system) sited between the two rows. The Mk 41 VLS adopts modular design concept, which result in different versions that vary in size and weight due to different "canisters" in various modules. The height (determining missile length) of the launcher comes in three sizes: 209inches for the self-defense version, 266inches for the tactical version, and 303inches for the strike version. The empty weight for an 8-cell module is 26800lbs for the self-defense version, 29800lbs for the tactical version, and 32000lbs for the strike version. Ticonderoga cruisers and Arleigh Burke destroyers up to DDG-78 have a Strikedown module fore and aft, which consists of five cells and a collapsible crane for assisting with replenishment at sea. As replenishment of large missiles at sea was later seen as impractical and dangerous, Strikedown modules fell out of use on newer ships.
The Mk 56 VLS is an evolution of the tactical length Mk 41 VLS which is a smaller version of the strike length Mk 41 used on s.
The Mk 57 Peripheral Vertical Launch System (PVLS) used on the s is composed of much larger VLS cells capable of venting much larger volume and mass of exhaust gasses (mass flow rate), but is an evolution of the smaller unarmored Mk 56 VLS. The Mk 57 PVLS are designed to be installed on the ship periphery with armor on the inboard boundary, instead of in centralized magazines used in the Mk 41.
Developed by Raytheon, Mk 57 provides backward compatibility with existing missiles while allowing new missiles with significantly increased propulsion and payloads. While allowing for larger missiles than the Mk 41, the primary improvement of Mk 57 is its exhaust gas management system which can accommodate new missile designs having up to 45 percent greater rocket motor mass flow rate than that of Mk 41.[12] The unique symmetric geometry of the U-shaped gas management system facilitates the egress of gases, while minimizing flow into adjacent cells and reversed flow into the active cell. Another advantage is the elimination of the water deluge system, which is used to cool the missile canister in the event that the missile restraint bolts do not release after rocket motor ignition. Elimination of the water deluge system significantly reduces maintenance and personnel requirements, and protects against accidental missile wet-down.
| Width | 7.25feet | |
|---|---|---|
| Length | 14.2feet | |
| Height | 26feet | |
| Weight | 33600lb | |
| Maximum canister width | 28inches | |
| Maximum canister length | 283inches | |
| Maximum canistered weight | 9020lb |
Germany
Japan
Spain
United States