WINDOW FOR AN AIRCRAFT, AIRCRAFT, AND METHOD FOR DETERMINING THE POSITION AT WHICH A LASER BEAM IMPACTS A WINDOW

The present invention is directed to a window (100) for an aircraft (10), the window (100) comprising a first transparent layer (110), and a first plurality of light detectors (111) arranged around a circumference of the first transparent layer (110) and configured to measure the intensity of light refracted upon entering and exiting the first transparent layer (110). Furthermore, the present invention is directed to an aircraft and a method for determining the point at which a laser beam (20) impacts a window (100) of the aircraft.