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RIM-161 Standard Missile 3

Stage 2: MK 104 Dual Thrust Rocket Motor (DTRM), solid-fuel, Aerojet Stage 3: MK 136 Third Stage Rocket Motor (TSRM), solid-fuel, ATK Stage 4: Throttleable Divert and Attitude Control System (TDACS), Aerojet • Service — 2014–present (Block IB) • Weight — 1.5 t • Length — 6.55 m • Diameter — 34.3 cm for Block I missiles 53.3 cm for Block II • Wingspan — 1.57 m • Speed — 3 km/s (Mach 8.8) Block IA/B 4.5 km/s (Mach 13.2) Block IIA • Vehicle Range — Block IA/B: 900 – Block IIA: 1,200 km range and flight ceiling 900 – 1,050 km (depending on the type of target) • Filling — Lightweight Exo-Atmospheric Projectile (LEAP) kinetic warhead • Guidance — GPS/INS/semi-active radar homing/passive LWIR infrared homing seeker (KW) The RIM-161 Standard Missile 3 (SM-3) is a ship-based surface-to-air missile used by the United States Navy to intercept ballistic missiles as a part of Aegis Ballistic Missile Defense System. The SM-3 has also been employed in an anti-satellite capacity against a satellite at the lower end of low Earth orbit. The SM-3 is primarily used and tested by the United States Navy and also operated by the Japan Maritime Self-Defense Force.

Also recorded as SM-3

RIM-161 Standard Missile 3

A Standard Missile-3 (SM-3) is launched from the guided missile cruiser USS Lake Erie (CG 70), during a joint Missile Defense Agency, U.S. Navy ballistic missile flight test. Approximately three minutes later, the SM-3 intercepted a unitary (non-separating) ballistic missile threat target, launched from the Pacific Missile Range Facility, Barking Sands, Kauai, Hawaii. Within moments of this launch

Lt. Chris Bishop Deputy Director, U.S. Navy photo (RELEASED) · Public domain

Name
RIM-161 SM-3
Field
anti-satellite weapon · anti-ballistic missile
Region
United States

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Stage 2: MK 104 Dual Thrust Rocket Motor (DTRM), solid-fuel, Aerojet Stage 3: MK 136 Third Stage Rocket Motor (TSRM), solid-fuel, ATK Stage 4: Throttleable Divert and Attitude Control System (TDACS), Aerojet • Service — 2014–present (Block IB) • Weight — 1.5 t • Length — 6.55 m • Diameter — 34.3 cm for Block I missiles 53.3 cm for Block II • Wingspan — 1.57 m • Speed — 3 km/s (Mach 8.8) Block IA/B 4.5 km/s (Mach 13.2) Block IIA • Vehicle Range — Block IA/B: 900 – Block IIA: 1,200 km range and flight ceiling 900 – 1,050 km (depending on the type of target) • Filling — Lightweight Exo-Atmospheric Projectile (LEAP) kinetic warhead • Guidance — GPS/INS/semi-active radar homing/passive LWIR infrared homing seeker (KW) The RIM-161 Standard Missile 3 (SM-3) is a ship-based surface-to-air missile used by the United States Navy to intercept ballistic missiles as a part of Aegis Ballistic Missile Defense System. The SM-3 has also been employed in an anti-satellite capacity against a satellite at the lower end of low Earth orbit. The SM-3 is primarily used and tested by the United States Navy and also operated by the Japan Maritime Self-Defense Force.

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wikidata · Q900937 · wikipedia · RIM-161 Standard Missile 3

In this article

  1. 01Origins and development
  2. 02Archives and collections
  3. 03Notes, references and evidence

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