The diagram illistrates about the basic engine structure of a rocket. It mainly reflects on the combusion method in rocket engines.
Overall, for rocket engines working, fuel and oxygen are needed to be combusted in a chamber. Then the remaining combustion products leave the chamber through a nozzle.
At the very beginning of the process, two tanks are needed to keep fuels and to hold oxygen. Then, the fuel is pumped with a pump from the tank. After that it is injected into the combusion chamber with the help of an injector. Similarly, Oxygen is thrown into the chamber after going through the oxydizer pump.However, after reaching the oxygen and the fuel in the chamber, they combust inside. This combusion mainly runs the engine. Lastly, the combustion products that have been originated as a by product is expeled along a nozzle at the end that is attached to the combusion chamber.
