9M83M/9M83ME
| Name | 9M83M/9M83ME |
|---|---|
| Image | ![]() |
| Varient | 9M83M 9M83ME |
| Country of origin | Russia |
| Type | Medium/Long range surface-to-air missile (SAM) |
| Range | 130-200 km (According to some other sources) |
| Altitude | 30 km |
| Length | 7.898 m |
| Diameter | 0.50 m |
| Fin span | 1.215 m |
| Mass | 1700 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 5-6 (Approx.) |
| Propulsion | Not known |
| Engine | Not known |
| Guidance | Inertial with semi-active radar terminal homing seeker |
| Launch platform | 50P6E transporter-erector-launcher |
| Service period | 1983-Present |
| Description | The 9M83M is a surface-to-air missile designed for the S-300V4 air defense system. It’s a versatile missile capable of engaging a wide range of aerial targets, including aircraft, drones, cruise missiles, and even ballistic missiles. The 9M83M features advanced guidance systems and a powerful propulsion system, enabling it to intercept targets at high altitudes and long ranges. This missile significantly enhances the S-300V4’s ability to counter modern aerial threats, making it a crucial component of the system’s layered defense capabilities. |
| Website | http://roe.ru/ |
Disclaimer: This information is based on publicly available sources and should be considered for general knowledge purposes only.
