Abstract: A high temperature capable probe housing for use in a gas turbine engine is disclosed. The rake is preferably made of silicon nitride or silicon carbide and is capable of withstanding the hostile environment within a gas turbine engine at temperatures greater than 1,200 Celsius while only passively cooled. The rake is a substantially elongated member extending between an at least partially open first end and a closed second end. The rake has an interior surface and an exterior surface. The interior surface defines an internal cavity beginning at the at least partially open first end and extending toward the closed second end. The exterior surface extends between the two ends and has a leading face having a plurality of openings upon which the flow generally impinges. The openings extend between the exterior surface and interior surface and are configured to receive a sensor.