“…In order to design an infrared imaging-based diagnostic system for use with turbojet engines and to construct a working knowledge base, a small iSTC-21v turbojet engine, developed in the Laboratory of Intelligent Control Systems of Aircraft Engines at the Faculty of Aeronautics, Technical University of Košice (Figure 9), was used [62]. This is a single-stream, single-shaft turbojet engine with a single-stage one-sided radial compressor, an annular combustion chamber, and a single-stage non-cooled gas turbine with a variable exhaust nozzle with full authority intelligent electronic digital control system developed from the TS-21 engine (Ljulka-Saturn, Rybinsk, Russia).…”