Abstract: Sight head with integrated laser designator for use in an aircraft such as a rotorcraft.
The laser designator (32) is integrated into a zone of a main external assembly of the pod (14) of the sight head (12), enclosed externally in an existing fairing (34). It comprises a laser transmitter (36), a power supply (38) and a radio receiver (40). The laser transmitter (36) is fitted to the site head structure using adjusting screws (46) which allows the alignment to be modified.