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The 9M133 Kornet (Russian: Корнет; "Cornet", NATO reporting name AT-14 Spriggan, export designation Kornet-E) is a Russian man-portable anti-tank guided missile (ATGM) intended for use against main battle tanks. It was first introduced into service with the Russian army in 1998. [6] The Kornet is among the most capable Russian ATGMs. [7]
Kornet-D is a Russian anti-tank missile carrier based on the AMS 233 144 TIGR-M 4x4 high mobility vehicle. It employs 9M133M Kornet-EM missiles in both tandem-HEAT or thermobaric warhead variants.
The 9M133M Kornet-M [2] (also known by the export designation 9M133 Kornet-EM) [1] Russian anti-tank guided missile (ATGM) is an improved version of the 9M133 Kornet ATGM, with increased range and an improved warhead.
The first man-portable rocket launcher to be mass-produced was the American 60 mm M1 rocket launcher, more commonly known as the bazooka. It was a man-portable, tube launched, recoilless rocket anti-tank weapon, widely fielded by the United States Army during World War II and into the Cold War.
An unguided surface-to-surface missile is usually referred to as a rocket (for example, an RPG-7 or M72 LAW is an anti-tank rocket), whereas a BGM-71 TOW or AT-2 Swatter is an anti-tank guided missile. Examples of surface-to-surface missile include the MGM-140 ATACMS and the Ground-Launched Small Diameter Bomb (GLSDB). [3] [4] [5] [6]
Shoulder-fired missile, shoulder-launched missile or man-portable missile, among other variants, are common slang terms to describe high-caliber shoulder-mounted weapons systems; that is, weapons firing large, heavy projectiles ("missiles"), typically using the backblast principle, which are small enough to be carried by a single person and fired while held on one's shoulder.
The 9K111 Fagot (Russian: Фагот; "bassoon") is a second-generation tube-launched semi-automatic command to line of sight (SACLOS) wire-guided anti-tank missile system of the Soviet Union for use from ground or vehicle mounts.
The Aerojet Rocketdyne AR1 is a 2,200-kilonewton-class (500,000 lbf) thrust RP-1/LOX oxidizer-rich staged combustion cycle rocket engine project. [1]The engine was conceived in 2014, and received US government funding to build a prototype engine in 2016. [2]