48N6E3/48N6DM (S-400)
| Name | 48N6E3/48N6DM (S-400) |
|---|---|
| Image |  |
| Varients | 48N6E3 48N6DM |
| Country of origin | Russia |
| Type | Long range surface-to-air missile (SAM) |
| Range | 240 km |
| Max altitude | 27 km |
| Length | 7.5 m |
| Diameter | 0.515 m |
| Fin span | Not known |
| Mass | 1835 kg |
| Flight Duration | Not known |
| Warhead | 180 kg |
| Warhead yield | Not known |
| Max Speed | Mach 5.9-6.5 Mach 14 (Terminal phase) |
| Propulsion | Not known |
| Engine | Not known |
| Guidance | Semi-active radar homing |
| Launch platform | 5P85TE2 transporter-erector-launcher/5P85SE2 on a trailer |
| Service period | 2007-Present |
| Description | The 48N6E3 is a long-range surface-to-air missile designed for the S-400 Triumf air defense system. It represents an enhancement over previous versions, boasting improved capabilities against ballistic missiles. The 48N6E3 features advanced guidance systems and a powerful propulsion system, enabling it to intercept targets at hypersonic speeds. This missile significantly enhances the S-400’s ability to counter advanced aerial threats, including ballistic missiles, aircraft, and drones, making it a crucial component of modern air defense systems. |
| Website | http://roe.ru/ |
Disclaimer: This information is based on publicly available sources and should be considered for general knowledge purposes only.