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RIM-162 ESSM

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RIM-162 ESSM
NameRIM-162 ESSM
CaptionAn ESSM launching from the USS *Fitzgerald*
TypeSurface-to-air missile
OriginUnited States
Used bySee #Operators
DesignerRaytheon
ManufacturerRaytheon
Production date2004–present
Service2004–present
EngineSolid-fuel rocket
Weight620 lb (280 kg)
Length12 ft (3.66 m)
Diameter10 in (254 mm)
SpeedMach 4+
GuidanceSemi-active radar homing / Inertial navigation system
Launch platformMk 41 Vertical Launching System, Mk 48 Vertical Launching System, Mk 29 Guided Missile Launcher

RIM-162 ESSM. The RIM-162 Evolved SeaSparrow Missile (ESSM) is a medium-range, surface-to-air missile system designed to defend naval vessels against advanced anti-ship missiles, aircraft, and surface threats. Developed as a significant upgrade to the RIM-7 Sea Sparrow, it features enhanced kinematics, a new airframe, and improved guidance for greater lethality and engagement flexibility. The system is a cornerstone of modern naval air defense, integrated into the Aegis Combat System and other platforms used by the United States Navy and allied fleets worldwide.

Development and design

The program originated from a NATO initiative in the late 1980s to develop a common next-generation missile to replace the aging RIM-7 Sea Sparrow. A consortium of nations, including the United States, Australia, Canada, Denmark, Germany, Greece, Netherlands, Norway, Spain, and Turkey, collaborated under the NATO Sea Sparrow Consortium. Primary design and integration work was led by Raytheon in the United States. Key design innovations include a larger, more powerful solid-fuel rocket motor and tail-controlled aerodynamic configuration for high maneuverability, enabling effective intercepts against high-speed, low-altitude threats like the P-800 Oniks. Guidance combines a mid-course update capability via Link 16 datalink with a terminal semi-active radar homing seeker, allowing for launch-and-leave engagements when cued by advanced radars like the AN/SPY-1.

Operational history

The missile achieved initial operational capability with the United States Navy in 2004, first deployed on *Wasp*-class vessels. It has since been integrated across numerous *Arleigh Burke*-class destroyers, *Ticonderoga*-class cruisers, and allied platforms like the Royal Australian Navy's *Hobart*-class. The ESSM has been a critical component of carrier strike group and expeditionary strike group defensive umbrellas during operations in the Persian Gulf, South China Sea, and Mediterranean Sea. It is routinely test-fired in major multinational exercises such as RIMPAC and Formidable Shield, demonstrating its interoperability within the NATO alliance. The Japan Maritime Self-Defense Force also employs the missile on its *Maya*-class vessels.

Variants

The primary production variant is the **RIM-162D (ESSM Block 1)**, which introduced the dual-mode semi-active seeker. The significant evolutionary step is the **RIM-162E (ESSM Block 2)**, currently in development, which incorporates an active radar homing seeker derived from the AMRAAM missile for full fire-and-forget capability, greatly enhancing engagement capacity against saturation attacks. Earlier variants include the **RIM-162A/B/C**, which featured incremental improvements in motor performance and guidance software. The missile is quad-packed in a single cell of the Mk 41 Vertical Launching System, dramatically increasing shipborne missile inventory compared to its predecessor.

Operators

* United States Navy – Primary operator across surface combatants and amphibious ships. * Royal Australian Navy – Equips the Hobart-class destroyer and Hunter-class frigate. * Royal Canadian Navy – For the Halifax-class frigate modernization and future Canadian Surface Combatant. * Royal Netherlands Navy and German Navy – For the Sachsen-class frigate and De Zeven Provinciën-class frigate. * Royal Norwegian Navy – Onboard the Fridtjof Nansen-class frigate. * Spanish Navy – Integrated on the Álvaro de Bazán-class frigate. * Additional operators include the navies of Denmark, Greece, Turkey, Japan, South Korea, Chile, and Poland.

Specifications

* **Length:** 12 ft (3.66 m) * **Diameter:** 10 in (254 mm) * **Weight:** 620 lb (280 kg) * **Warhead:** Blast-fragmentation * **Propulsion:** Single-stage, high-impulse solid-propellant rocket motor * **Speed:** Greater than Mach 4 * **Range:** In excess of 50 km (27 nautical miles) * **Guidance:** Mid-course update via datalink (e.g., Link 16), terminal semi-active radar homing (Block 1); active radar homing (Block 2) * **Launch Systems:** Compatible with Mk 41 Vertical Launching System, Mk 48 Vertical Launching System, and the Mk 29 Guided Missile Launcher.

Category:Surface-to-air missiles of the United States Category:Naval missiles Category:NATO