48N6D/48N6E2 (S-400)
| Name | 48N6D/48N6E2 (S-400) |
|---|---|
| Image | ![]() |
| Varients | 48N6D/48N6E2 |
| Country of origin | Russia |
| Type | Medium range surface-to-air missile (SAM) |
| Range | 200 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 |
| Detonation Mechanism | Radio proximity |
| Max Speed | Mach 5.9 Mach 8.2 (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 | 2004-Present |
| Description | The 48N6E2 is a long-range surface-to-air missile designed for the S-400 Triumf air defense system. It possesses a significant range, allowing it to engage a wide array of aerial targets, including aircraft, drones, and ballistic missiles, at considerable distances. The 48N6E2 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-400’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.
