Delilah Israel Cruise Missile

The Delilah missile is a cruise missile developed in Israel by Israel Military Industries (IMI), built to target moving and re-locatable targets with a CEP of 1 metre (3 ft 3 in). The Delilah cruise missile is the name of several variants of an Israeli missile built by IMI (formerly TAAS). It was originally developed as an aerial decoy, but evolved into an offensive strike weapon in the 1990s used by Israel F-16's and upgraded F-4E attack aircraft.

Delilah cruise missile

Delilah is an air-launched stand-off and cruise missile, with a turbo jet engine that allows the ability to loiter in order to enable it to target well-hidden threats, as well as attack moving targets, making it ideal in destroying SAM threats. It has a range of 250 km, and can destroy targets both on sea and on land. An autopilot onboard as well as an INS/GPS navigation system allows the missile to perform its mission autonomously; a data link enables intervention and target validation. The missile can be fitted with a variety of warheads and can be fitted to most aircraft.

It can be fired from aircraft, helicopter, or ground launcher. Its compact dimensions allow it to be carried by the Sikorsky UH-60A and SH-60B helicopters. It carries a small but effective warhead to allow it to destroy the target but minimize collateral damage.

This missile was first used in combat by Israel over Lebanon on July and August 2006, launched by an F-16D fighter aircraft.

The Delilah-GL is a ground-launched variation of the Delilah cruise missile, that has a range of 250 km. It is equipped with a 30 kg conventional explosive warhead but is capable of carrying 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.

Delilah missile
Type	Cruise missile
Place of origin	Israel
Service history
In service	1995-
Used by	Israel
Production history
Manufacturer	Israel Military Industries
Specifications
Weight	250 kilograms (550 lb)
Length	3.31 metres (10.9 ft)
Diameter	0.33 metres (1 ft 1 in)
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