This document summarizes the key components and operation of a gas turbine. It describes the main elements as the air intake, compressor, combustion chamber, expansion turbine, and rotor. It explains that air is compressed in the compressor before being mixed with fuel and burned in the combustion chamber. The hot gases then expand through the turbine to produce rotational energy. Gas turbines have advantages like being very light, easy to maintain, suitable for automation, and small/easy to start. They are commonly used for electricity generation and ship/aircraft propulsion. While capital efficient, their historic disadvantage was low efficiency, but modern turbines have addressed this issue.