Process for operating a reaction-type missile propulsion system and missile propulsion system

摘要

A method for accelerating a vehicle in the atmosphere, space or aerospace includes the steps of supplying a propellant having silicone hydride compounds into a combustion chamber, compressing air and delivering compressed air into a ring formed with a plurality of circumferential orifices which open into the combustion chamber, reaching thereby temperatures of about 3000 C., cracking nitrogen molecules present in the air at the temperature which attack the silicon atoms to generate great mass.