Nimrod (missile)

From Wikipedia, the free encyclopedia
Jump to: navigation, search
Nimrod missile in Paris Air Show

Nimrod is a long-range air-to-surface and surface-to-surface missile developed by Israel Aerospace Industries. While primarily designed for anti-tank use, it provides standoff strike capability against a variety of point targets such as APCs, ships, bunkers, personnel concentrations and guerrillas.

Nimrod has a semi-active laser guidance system, capable of day and night operation. Its flight trajectory can be set below obscuring cloud layers, while a forward scouting team uses a laser designator to direct it from up to 26 km behind.

Nimrod may be installed on a variety of towed launchers, light combat vehicle launchers, helicopters, and fixed-wing aircraft. The primary helicopter launch platform for the Nimrod in the Israel Defense Forces is a modified CH-53 helicopter; this is not only due to the relatively large size and weight of the Nimrod missile, but because the CH-53 is a common delivery vehicle for Israeli special operations teams. The launching vehicle or aircraft may fire up to 4 Nimrods at once from a single pack.

Development/Description[edit]

Israel Aircraft Industries MBT Weapon Systems Division has developed the solid propellant fuelled day/ night-capable Nimrod long-range ground-launched semi-active laser-guided Anti-Tank Guided Weapon (ATGW) in response to an export requirement. Israeli Defence Force has also expressed interest. Nimrod can also be used as an anti-ship weapon.

Nimrod is transonic in operation and is powered all the way to the target. The gunner preselects the flight trajectory mode. This can be direct trajectory, high cruising trajectory or low cruising trajectory, the cruising altitude being constant and between 300 and 1,500 m. Mid-course guidance is provided by an integral inertial platform, and terminal guidance by a semi-active laser homing seeker for the last 15 to 30 seconds of missile flight. The target can be illuminated either by a ground-based or airborne laser designator.

The gimballed and stabilised seeker head acquires, tracks and homes in on its target using localised proportional navigation. It is said to have a look angle of more than 30°. The seeker has a search area of 5 km in width and 5 km in depth. In the terminal flight phase the weapon adopts a dive angle of approximately 45° to impact the armoured target on its vulnerable upper surfaces.

The missile is stored in a sealed canister which also acts as the launcher. Total weight of the missile and canister is 150 kg. It has five main sections: seeker, guidance and control, warhead, solid propellant rocket motor and servo. It is roll-stabilised in flight. Time to come into action at a launch site is less than 3 minutes without the site having to be surveyed for alignment or levelling, or with a direct line of sight to the target. The weapon can be fired in single-round, ripple or salvo modes.

In addition to the AMX-13 light tank tracked chassis application mentioned below there is also a truck (4 x 4) model with a pod of four missiles in the ready to launch position at the rear firing over the cab. Modified AMX-13 light tank chassis (two eight-round container-launcher installations - unknown export customer).

Production complete. In service with an unidentified export customer. Recent information has indicated that Nimrod may be in service with the Israel Defence Force with target acquisition being carried out by special forces.

Versions[edit]

Currently two versions of Nimrod exist:

  • Long Range, Dual Mode Missile – NIMROD 2 A dual mode Laser/GPS Homing missile, the Nimrod 2 has a range of 36KM and features a mobile launcher. The warhead is 14kg, and the missile can support various warheads for a variety of targets.
  • Long Range, Dual Mode Missile – NIMROD 3 A dual mode Laser/GPS Homing missile, the Nimrod 3 has a range of 10-50KM and can support various warheads for a wide range of targets. It also has a mobile launcher.

Operators[edit]

 Israel
 Colombia

Characteristics[edit]

  • Effective range: 300 - 36,000 meters
  • Length: 265 cm
  • Diameter: 170 mm
  • Body: 18 cm
  • Span 40 cm
  • Weight: 100 kg
  • Speed: ~2000 km/h Or Mach 0.8
  • Propulsion: Single stage solid rocket motor
  • Guidance: Semi-Active Laser Homing
  • Warhead: HEAT, Fragmentation-HE, Thermobaric, Anti Personnel Munition

See also[edit]

  • LAHAT, dubbed Nimrod-SR for the Latin American market.[1]

Comparable systems[edit]

References[edit]

External links[edit]