In an ideal gas turbine, gases undergo four thermodynamic processes: isentropic compression, isobaric (constant pressure) combustion, isentropic expansion, and heat rejection. Together these make up the Brayton cycle.In a real gas turbine, when gas is compressed (in a centrifugal or axial compressor

As a power source[edit]The V-2 rocket uses hydrogen peroxide decomposed by a liquid sodium permanganate catalyst solution as a gas generator. This is used to drive the turbo pump to pressurize the main LOX-ethanol propellant. [1] In the Saturn V F-1[2][3] and Space Shuttle main engines,[4] some prim

Generally, turbo-generators are not prone to failure under the correct use and maintenance, but if they are improperly used and maintained, the environment is poor, and they are in disrepair for a long time, they will also cause failures.