9M82

SAM 9M82 is intended for use as part of the S -300V air defense system and provides for the destruction of aerodynamic and ballistic air targets in the range of the complex. The composition of the missile system includes a launch vehicle 9Y238, a gas generator container 9D152 and the 9M82 rocket itself. The 9M82 rocket has two stages and is made according to the “bearing cone” scheme. The main parts of the rocket include: a glider, a propulsion system, a gas-hydraulic system, a separation system, electrical equipment, on-board equipment and a warhead ^[1] .

9M82 has two firing modes: single launch and a salvo of two missiles. In volley mode, the second missile launches in 1.5-2 seconds after the launch of the first. Missiles are launched from a transport and launch container mounted on a launch or launch loading launcher at a 90 ° angle. The rocket is pushed out of the container using a gas generator. For the safety of the launcher during the launch of the rocket launch engine, after departure from the container, the rocket preliminarily declines toward the bow of the launcher. Then, the starting engine starts and the missiles are guided at the angles of the optimal flight path to the target location zone. The starting engine runs from 3.5 to 6.2 seconds. The final guidance on the target occurs after separation of the launch stage. The main engine runs from 11.16 to 17.21 seconds ^{[2] [1]} .

Aiming at the target occurs in two modes. The first is inertial guidance with guidance in the final section. In this mode, on-board equipment of the rocket receives information about the speed characteristics of the target and its position. The second mode is a command-inertial control method with subsequent guidance. In this mode, the missile receives information about the relative position of the missile and the target, as well as about its speed characteristics. This mode is used in the jamming area. If the launcher detects interference directors, the information is transmitted to the guidance station, where the station commander selects the guidance method. When the required distance to the target is reached, the missile captures the target with homing equipment and is deployed in the immediate vicinity for the maximum effect of the directed warhead. An explosive device 9E322 produces a command to detonate the warhead when a reflected signal from a target appears in the receiver. If the rocket flies past the target, then self-destruction is carried out ^[3] .

The main elements of the starting stage are the starting engine and the tail compartment. To give the thrust vector, four rotary valves are installed on the engine nozzle. On the outside of the starting engine laid electric lines for communication between the equipment of the detachable part ^[4] .

The marching stage is divided into eight compartments. DB100M guidance equipment, a radio block of an explosive device, a navigation device for an inertial control system and an on-board computer are installed in the head part. In the tail part there is a gas turbine power supply unit with a gas-hydraulic system of the marching system. A self-liquidation system was also installed there. In front of the marching engine is a warhead with a safety-executive mechanism. Cable lines for connecting the tail and the head of the rocket are laid along the outer surface of the marching engine ^[4] .

9M82M

9M82M - anti-aircraft guided missile anti - aircraft missile system 9K81M "Antei-2500" . The range of the missile rocket has been significantly increased and amounts to 200 km. The missile is capable of hitting targets maneuvering with overloads up to 30g. The maximum flight speed was also increased and amounts to 2600 m / s ^[5] .

9M82ME - export version

• 9M82.0000TO. Product 9M82. Technical description. - 1984 .-- 107 p.
• Davydov M. V. Part 2. Anti-aircraft missile systems // Years and People. - (from the history of NIEMI, electronic version of the publication with corrections and additions made in the period 2002-2010). - Moscow: Radio and Communications, 2009. - ISBN 5-256-01601-6 .

• Anti-aircraft guided missiles 9M82 (9M82M) and 9M83 (9M83M) (Russian) . Missile technology (July 28, 2010). Date of treatment January 21, 2012. Archived May 18, 2012.
• C-300V - 9M83 and 9M82 anti-aircraft guided missiles (Russian) . Bulletin of air defense (02/11/2001). Date of treatment January 21, 2012. Archived May 18, 2012.