9M82M/9M82ME
| Name | 9M82M/9M82ME |
|---|---|
| Image | ![]() |
| Varient | 9M82M 9M82ME |
| Country of origin | Russia |
| Type | Long range surface-to-air missile (SAM) |
| Range | 200-250 km |
| Altitude | 30 km |
| Length | 10.525 m |
| Diameter | 0.85 m |
| Fin span | 0.915 m |
| Mass | 3300 kg |
| Flight Duration | Not known |
| Warhead | 150 kg, HE focused fragmentation with selectable in-flight proximity fuzing capability |
| Warhead yield | Not known |
| Max Speed | Mach 7.0-8.0 (Approx.) |
| Propulsion | Solid rocket |
| Engine | Solid rocket motor |
| Guidance | Inertial with semi-active radar terminal homing seeker |
| Launch platform | 50P6E transporter-erector-launcher |
| Service period | 1983-Present |
| Description | The 9M82M is a long-range, surface-to-air missile designed for the S-300V4 air defense system. It possesses a significant range, allowing it to engage a wide spectrum of aerial targets, including aircraft, drones, cruise missiles, and even ballistic missiles, at considerable distances. The 9M82M incorporates advanced guidance systems and a powerful propulsion system, enabling it to effectively intercept targets with high accuracy. It plays a crucial role in enhancing the S-300V4’s capabilities to counter modern aerial threats, making it a formidable component of the air defense system. |
| Website | http://roe.ru/ |
Disclaimer: This information is based on publicly available sources and should be considered for general knowledge purposes only.
