A thrust reverser for a turbojet engine includes a telescopic linear actuator for a moving cowl and a nozzle-forming end part. The first and second temple pieces each include an adjustment mechanism for adjusting the length and angle of the first and second temple pieces. An associative lookup is performed in a map index using the fully qualified hashing code. The plurality of outer core portions and a plurality of the magnets are alternately arranged in the circumferential direction. The at least one dynamic seal extends between the sump housing and the rotating structure to isolate the high-momentum lubricant flow from the low-momentum lubricant flow.