Combustion chambers in various types of jet engines. Jet Engine Type Combustion Chamber Type Description Materials Used Advantages Disadvantages Turbojet Can-type Individual, separate combustion chambers (one per fuel nozzle). Nickel-based superalloys (Inconel, Hastelloy), stainless steel. Easy maintenance, modular design. Heavier, bulkier, inefficient airflow. Turbofan Annular A single continuous ring-shaped chamber surrounding the engine core. Nickel-based alloys (Rene 41, Hastelloy X), ceramic coatings for heat resistance. Efficient fuel-air mixing, compact, lighter. More complex to manufacture, difficult to maintain. Turboprop Can-annular A mix of can-type and annular designs: multiple cans inside an annular outer shell. Cobalt...
“Defying gravity: How heavy metal flew and changed aviation forever.