| 摘要 |
The launcher (2) has a sensor unit (5) detecting a missile, and a launching unit (6) for launching the missile detected by the sensor unit. The unit (6) is arranged at a rotating unit (4), such that the unit (6) is rotatable around a horizontally running elevation axis by an electric motor drive (10). The unit (4) is arranged opposite to a mounting unit (3), such that the unit (4) is rotatable around a vertically running azimuth axis by another electric motor drive (20). A decoupling unit decouples the rotating movement of the unit (4) from the rotating movement of the unit (6). |
