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 ...

The thrust chamber - consisting of the injection head, combustion chamber and expansion nozzle - as part of a rocket engine is one of the most thermally and mechanically stressed parts of a rocket and ...

from industrial burners to rocket engines. Recent studies have employed advanced numerical simulations to explore the flow dynamics in vortex combustion chambers. For instance, one study utilized ...

Liquid-fuelled rocket engine design has largely followed a ... Propellant and oxidizer are mixed in a combustion chamber, creating a mixture of hot gases at high pressure that very much wish ...

A team of University of Bristol students have designed, built, and tested a rocket engine to 6000 Newtons – roughly the same ...

An artificial intelligence engineer called Noyron has successfully designed, manufactured, and tested one of the most challenging rocket engines ... outside of the combustion chamber, which ...

“The final test achieved a fantastic 6,000 Newtons of thrust, breaking the previous record set by the University of Sheffield ...

Credit: SpaceX When a chemical rocket engine fires, it's the purest expression ... With a powerful turbopump, the combustion chamber can be supplied with more or less fuel to change the thrust ...

3D printing is an incredible tool for prototyping and development, but the properties of the materials can be a limiting factor for functional parts. [Sam Rogers] and colleagues at [AX ...