Abstract:
A package, able to encapsulate at least one component, forming a closed cavity of Faraday cage type having side walls resting on a base and that are surmounted by a cover, wherein at least one of the side walls includes exterior electrical connection elements linked electrically to the interior of the cavity, the exterior connection elements able to interconnect with an exterior circuit such that the side wall faces the exterior circuit when the exterior connection elements are interconnected with the circuit.
Abstract:
A probe system, mixed primary reference probe for an aircraft, associated aircraft and measuring method are disclosed. In one aspect, the probe system includes a base designed to be fastened on the cockpit of an aircraft, a plurality of regularly spaced static pressure taps, arranged through the base and designed to be connected to a pressure measurement device. The system includes at least one optical window transparent to laser radiation and inserted into the base.