For example, the typical heat flux density values for the Vulcain engine with a combustion chamber pressure of 10.5 megapascals (MPa) are up to 80 MW/m 2 and for the space shuttle main engine at 20.5 ...

The new Vulcain 2.1 engine ... the development engines must prove that they can cope with the enormous thrust of 130 tons, temperatures of around 3000 degrees Celsius in the combustion chamber, the ...

Rocket engines consume an immense amount of fuel and oxidizer, and powerful pumps are required to get the propellants injected into the combustion chamber at the necessary pressure. To power these ...