SOM (missile)

SOM Cruise Missile
SOM cruise missile mockup exhibited during MSPO 2014 at Kielce, Poland.
Type	Cruise missile Anti-ship missile
Place of origin	Turkey
Service history
In service	Since 2012
Production history
Manufacturer	TÜBİTAK-SAGE and Roketsan SOM-J to be additionally produced by Lockheed Martin under licence from Roketsan
Specifications
Weight	600 kilograms (1,323 lb)
Length	3,657 millimetres (12.0 ft)
Warhead	230 kilograms (507 lb) SOM-A: High Explosive SOM-B1: High Explosive SOM-B2: Dual-stage penetrator SOM-J: Semi-armour piercing type with blast/fragmentation
Engine	Microturbo TRI 40 2.5-3.3 kN
Wingspan	2,600 millimetres (8.53 ft)
Operational range	250 km (130 nmi) (operational variant)
Flight altitude	Terrain hugging Sea skimming
Speed	623 knots (0.94 Mach )
Guidance system	INS / GPS Terrain Referenced Navigation Image Based Navigation Automatic Target Recognition Imaging Infrared Seeker
Accuracy	5 metres (16 ft) CEP
Launch platform	F-16 Fighting Falcon F-4 Phantom II F-35 Lightning II

External image

Launch and Warhead test

SOM-B1 Test

SOM Cruise Missile (Turkish: Satha Atılan Orta Menzilli Mühimmat) is a next-generation high precision cruise missile, which can be launched from land, sea and air platforms developed by TÜBİTAK SAGE, Defence Research and Development Institute of Turkey. It was first revealed during the 100th anniversary celebrations of the Turkish Air Force at the Çiğli Air Base in İzmir, on 4 June 2011. Developed since 2006, the SOM cruise missile is Turkey's first domestic solution for destroying both stationary and moving targets at a stand-off distance of over 180 kilometers. Although being developed by TÜBİTAK SAGE which still holds authority over the design of the missile, Roketsan has been given the role of producing and marketing the missile for export.

The SOM stand-off cruise missile is a family of launch and leave precision strike weapons against both land or sea targets. It uses GPS as its primary mode of guidance complemented by an advanced Inertial Navigation System and a radar-based Terrain Referenced Navigation system, allowing the missile to skim the terrain during its flight in order to evade local defence systems. According to the developer, it features advanced geometry and aerodynamics over similar missile systems, as well as lightweight composite components that minimize the radar cross-section of the missile. A terminal stage infrared imager detects the individual target by matching its signature with a pre-loaded database of similar targets allowing for precision strike. It can also be used to provide image-based midcourse navigation by taking snapshots of waypoints and comparing them against predicted position to update the navigation system. By this way, if GPS capability is denied or degraded, the missile can follow its waypoints using infrared based terrain updates. The missile includes a two-way datalink that makes possible to change the task in flight.