State trials of the new Russian short-range Sosna missile defense system will begin in early 2016 so that the Russian Defense Ministry can deliver the complex by the middle of the year, a deputy head of the system’s designers said Wedesday.
The system is intended to protect against all types of air threats including high-precision weapons e.g. cruise missiles and guided aircraft missiles in the area of the system responsibility: in range – up to 10 km, in altitude – up to 5 km.
Structure principles
• mount of missile armament with a launcher in one combat vehicle, air search and target tracking equipments, missile flight control units that are combined by integrated optronic combat control system
• missile armament consists of 12 high-speed high-precision maintenance-free missiles SOSNA-R deployed in a launcher. Light weight of the missiles allows to dispose of a transport/loading vehicle from the system
• optimal configuration of surface-to-air guided missile (SAM) payload allows to improve impact effect due to increased weight of spread warheads and application of impact/non-impact laser fuse with continuous circular beam pattern and adaptive burst time
• special multichannel automatic high-precision practically all-weather and day/night optronic control system
• combined missile control system:
– radio command system in start zone
– remote orientation in laser beam after engine division and missile targeting to the line-of-sight
• optronic combat control system with sector scan and in the automate target designation mode provide autonomous target detection capability
Qualities
• high effectiveness of combat application including high-speed and low-flying targets and helicopters during pop-up maneuvers
• high automation of combat processes
• day/night and all-weather capability of combat processes
• concealed fire preparation and high survivability
• unlimited minimum flight altitude of hitting target
• radar and optical countermeasure equipments immunity
• capacity to firing on the move
| Performance characteristics | |
| armament | SAM “Sosna-R”, 12 pcs. |
| missile weight at launch, kg | 30 |
| missile weight in TLC, kg | 42 |
| caliber before / after SAM detachment, mm | 130 / 72 |
| maximum velocity, m/s | 900 |
| guidance system | combined |
| engagement zone, km | |
| in range | up to 10.0 |
| in altitude | up to 5.0 |
| day / night use | available |
| time | |
| reaction, s | 5.0 – 8.0 |
| reloading, min | 10.0 |
| operating mode | autonomous and centralized control |