Title: Name: | 9M133F Kornet | 9M133F Kornet |
Original title: Original Name: | 9М133Ф Корнет | |
Manufacturer: Producer: | DD.MM.1998-DD.MM.YYYY Děgťarjova factory, Kovrov | |
Period of production: Production Period: | DD.MM.1998-DD.MM.YYYY | |
Made pieces: Number of Produced: | ? | |
a Prototype made: Prototype Built: | DD.MM.1994 | |
Use: Use: | 9K128 Cornet-With 9K128-1 Cornet-T 9K129 Cornet-P 9K130 9K131 Kliver 9K135 Vesť 9K??? Quartet 9K??? Kornet-D 9K??? Kornet-EM 9K??? Cornet-D1 | |
Technical data: Technical Data: | ||
the Weight of the projectile: Missile Weight: | 261) kg | 571) lb |
the Weight of the warhead: Warhead Weight: | ? kg | ? lb |
Length: Length: | 1200 mm | 3 ft 11 ¼ in |
body Diameter: Diameter: | 152 mm | 6 inches |
wingspan: Wingspan: | 460 mm | 1 ft 6 ⅛ in |
Way to guide: Guidance System: | a Semi-automatic method to guide - laser beam (SACLOS) | Semi Automatic Command to Line Of Sight - laser beam(SACLOS) |
Drive: Propulsion: | ||
Type: Type: | rocket engine solid fuel | a Solid-fuel rocket |
Feats: Performance: | ||
Speed: Speed: | 900 km/h | 559 mph |
Range: Range: | 5.5 km | 3 me |
Note: Note: | Code NATO: AT-14 Spriggan Termobarická hlavica, the equivalent of 10 kg of TNT Exportná verzia: 9M133F-1 Kornet-E 1)hmotnosť rockets with kontajnerom 29 kg | NATO designation: AT-14 Spriggan Thermobaric Export version: 9M133F-1 Kornet-E 1) 64 lb with launch tube |
Source: Sources: | https://en.wikipedia.org/wiki/9M133_Kornet www.russianarms.ru |