Offline
Investigations revealed that compressor blade failure was the cause of a few engine FOD damage cases. As the engine was manufactured in the early years, the compressor blades are no longer in production. The cost of maintenance for this engine is also too high. Hence, it was decided to replace the engine with a new state of the art turbojet engine.

You have been tasked to evaluate some of the latest models of turbojet engines and present your findings and reccomendations. The engine must be capable of producing 15 000 lbs of take-off thrust: