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Delilah (missile)

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Delilah missile
Delilah missile side.jpg
Type Cruise missile / loitering munition
Place of origin Israel
Service history
In service 1980s (initial versions, limited use), fully operational 1995-present
Used by See users
Production history
Manufacturer Israel Military Industries
Specifications
Weight 187 kilograms (412 lb)
Length 2.71 metres (8 ft 11 in)
Diameter 0.33 metres (1 ft 1 in)
Warhead weight 30 kilograms (66 lb)

Wingspan 1.15 metres (3 ft 9 in)
Operational
range
250 kilometres (160 mi)
Flight altitude 28,000 feet (8,500 m)
Speed Mach 0.3-0.7 (Dive: Mach 0.85)
Guidance
system
CCD\IIR with GPS\INS
Accuracy 1 metre (3 ft 3 in) CEP
Launch
platform
aircraft, helicopter, ground launcher, sea launcher

The Delilah missile is a cruise missile or loitering munition[1] developed in Israel by Israel Military Industries (IMI). The missile is designed to target moving and re-locatable targets with a circular error probable (CEP) of 1 metre (3 ft 3 in). Unlike a typical cruise missile, which is locked onto a pre-programmed target prior to launch, the Delilah missile's unique feature, as claimed by the manufacturer, is being able to loiter and surveil an area before a remote weapon systems officer, usually from the launching fighter aircraft, identifies the specific target of the attack.[2][3]

Overview[edit]

The name Delilah had been used by an anti-radiation attack drone configured after the US MQM-74 Chukar aerial target. It entered service in IAF in the mid-1980s. This air-launched drone identifies radar sites, allowing them to be found and destroyed. The Delilah missile is the name of a missile family built by IMI. Delilah was initially created as an aerial decoy, and was later developed into an offensive strike weapon in the 1990s used by Israeli F-16 and upgraded F-4E attack aircraft. It is multi-platform and has multi-target capability. Its uses include Air-to-Surface (AS), Surface-to-Surface (SS), Air-to-Air (AtoA), and Surface-to-Air (SA), targeting ground targets, vehicles and sea vessels, either stationary or moving. It is classed as a Medium Range, Multi-Purpose Guided Missile (MRMPGM), as All-in-One. It was Combat-Proven in Lebanon by Israeli Forces.

The Delilah is an air-launched stand-off missile and cruise missile with a range of 250km. It can be fitted with a variety of warheads which can be targeted on both land and sea targets. It has a turbo jet engine that is able to loiter, allowing it to target well-hidden threats in addition to moving targets. Its maneuverability makes the missile ideal for destroying surface-to-air missile threats. The on-board autopilot and inertial navigation-global positioning navigation systems (INS/GPS) allow the missile to perform its mission autonomously. A data link enables intervention and target validation. The Delilah missile was first used in combat by Israel over Lebanon in July and August 2006 and launched by F-16D fighter aircraft. The missile can be fired from most aircraft, helicopters, or ground launchers. Its compact dimensions allow it to be carried by the Sikorsky UH-60 Black Hawk and SH-60B helicopters.

Delilah-GL Missile[edit]

The Delilah-GL is a ground-launched version of the Delilah cruise missile, that has a range of 250 km. It is equipped with a 30 kg conventional explosive warhead. the missile can also be modified to carry other payloads, such as infrared target seeking and guidance devices. It is guided by GPS and has the ability to loiter in the target area, before confirming the target through real-time visual intelligence.

Operators[edit]

Current operators[edit]

References[edit]

  1. ^ Delilah – The IAF Loitering Missile, Defense Update, June 2009
  2. ^ "5 More Incredible Technologies Used by the IDF". idfblog.com. 19 January 2012. Retrieved 29 April 2017. 
  3. ^ The Secrets of Delialah, IAF bulletin, issue 184, December 2008

External links[edit]