In order to significantly increase the effectiveness, performance and specific impulse of future rocket engines, high combustion chamber pressures are required above all. If the combustion chamber ...

From a thermodynamic point of view, detonations are more efficient than the more commonly known deflagration (classic combustion ... chamber at high frequency and thus generate quasi-stationary thrust ...

Propellant and oxidizer are mixed in a combustion chamber, creating a mixture of hot gases at high pressure that very much wish to leave out the back of the rocket, generating thrust. However ...