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SOM (missile)
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SOM (missile) : ウィキペディア英語版
SOM (missile)

SOM Cruise Missile () is a next-generation high precision cruise missile, which can be launched from land, sea and air platforms〔(【引用サイトリンク】title=Turkey finalizes 200 km range missile tests - BUSINESS )〕 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.〔(【引用サイトリンク】url=http://www.sage.tubitak.gov.tr/sage_content_files///projeler/som/tubitak_sage_som_foy_050511.pdf )〕〔(Turkey reveals stand-off missile bunker buster ). ''TRDefence''. Retrieved 6 June 2011〕 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.〔 ''David Donald'' (UAE is first export success for CIRIT ). ''Jane's''. Retrieved 20 February 2013〕
==Description==
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.〔〔 ''Uğur Cebeci, Tolga Özbek (DHA)'' (Yerli seyir füzesi, 180 kilometreden hedefini vuracak ). ''Hurriyet''. Retrieved 6 June 2011〕〔(Turkey’s Stand-Off Missile is revealed ). ''Janes's DSEi2011 Exhibition News''. 14 September 2011〕
Basic design of the missile incorporates dedicated fuselage that fits in the internal bays of the Joint Strike Fighter.〔
It is intended to achieve high accuracy in striking military targets like command and control facilities, SAM sites, parked aircraft and surface ships.〔(DSEi: Turkish cruise missile design breaks cover ). ''Flight Global''. 14 September 2011〕


抄文引用元・出典: フリー百科事典『 ウィキペディア(Wikipedia)
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