Liquid-Fuel Rocket: XLS-191

Parts for a small liquid fueled rocket engine that I designed using equations from "How to Design, Build and Test Small Liquid-Fuel Rocket Engines." Would burn kerosene and LOX at 0.75 lb/sec at a mixture ratio of 2.2 and a thrust of 191 lbs. ISP of 255 seconds. Plan is to make molds of the printed parts and then cast them out of metal.

The combustion chamber is the major component of this engine, it is encapsulated by two cooling jackets which run kerosene along the outside of the combustion