Abstract: Disclosed are embodiments of a drone with a flattened tubular part protrudingly mounted on a module located on the fuselage of the drone, where the free distal end of the drone may also include a Pitot tube dynamic pressure front air intake. An internal duct may further connect the air intake to a pressure sensor mounted on the module. The tubular part may be mobile with respect to the module and may further include a means or mechanism for the mechanical coupling to a contractor mounted on the module. The tubular part may further include a light guide in light communication with a luminescent element mounted in the vicinity or at the level of the proximal end thereof. The tubular part may also include two sectionalized portions that are nested and in continuation of each other, where the base portion may be permanently linked to the module and a removable protruding portion may be located at the top base portion, which may include a front air intake and an internal duct.