48N6E
| Name | 48N6/48N6E |
|---|---|
| Image |  |
| Varients | 48N6 48N6E |
| Country of origin | Russia |
| Type | Medium range surface-to-air missile (SAM) |
| Range | 5-150 km |
| Max altitude | 27 km |
| Length | 7.5 m |
| Diameter | 0.519 m |
| Fin span | 1.134 m |
| Mass | 1800 kg (Approx.) |
| Flight Duration | Not known |
| Warhead | 143 kg, High explosive fragmentation |
| Warhead yield | Not known |
| Detonation Mechanism | Radio proximity |
| Max Speed | Mach 5.9-6 |
| Propulsion | Not known |
| Engine | Not known |
| Guidance | Inerital guidance system, Semi-active radar homing (Terminal phase) |
| Launch platform | 5P85TE2 transporter-erector-launcher/5P85SE2 on a trailer |
| Service period | 1992-Present |
| Description | The 48N6 missile is a long-range surface-to-air missile designed for the S-400 Triumf air defense system. It employs a combination of inertial guidance and active radar homing for precise target engagement. With a range of around 150 kilometers, it can intercept a variety of aerial targets, including aircraft, drones, and cruise missiles. |
| Website | http://roe.ru/ |
Disclaimer: This information is based on publicly available sources and should be considered for general knowledge purposes only.