PROCESS FOR IGNITING A ROCKET ENGINE AND ROCKET ENGINE

摘要

A process for igniting a rocket motor or a rocket engine with a free, molecular oxygen containing hot gas obtained by decomposing at least one ignition system liquid (1) is presented.The rocket motor contains a fuel rich propellant mixture based on fuel and oxidizer, the fuel in the mixture being selected from the group of aluminium, HTBP, GAP, Poly Nimmo and BAMO.The rocket engine uses fuel rich streams of propellant, which streams of propellant are based on a combination of fuel and oxidizer, said fuel being selected from the group of hydrogen, methane and kerosene.