Good on you and your mate, mate!<br /><br />Takes me back to the early 1960's when I was designing and static testing 55 lbf fuming nitric acid/analine rocket engines. They were uncooled, as the propellant flow rates weren't high enough to have permitted regenerative cooling without boiling the propellant being used for cooling. A larger one (in the 200 lbf) class could have been regeneratively cooled, but I started college right after the last series of static tests, and never had access to a test facility like the one I was able to get to use at a well-known university. (I didn't attend there, unfortunately!)<br /><br />To keep the combustion chamber and nozzle from burning up, I utilized Hastelloy C and Hastelloy X, and had the same outfit that coated the XLR-99 for the X-15 flame-spray a layer of zirconium oxide on the inside surfaces.<br /><br />I poured over a book called, "Rocket Combustion Elements" by George P. Sutton, while in high school. The school was tolerant in allowing me to do small experiments with Red Fuming Nitric Acid and analine in the chem lab. (The lab had high ceilings!) Experimented with mixture ratios poured into steel cans. Took LOTS of precautions. This propellant combination was well-known and had fewer potential hazards than LOX in handling. All you had to do was avoid inhaling the fumes, and keep your skin protected. Although LOX (LO2) is non-toxic, all it takes is the presence of a very small amount of hydrocarbon to cause a nasty explosion. Therefore, connector threads, pipes, tubing, etc., must be thoroughly decontaminated from any oils that were used in the manufacturing process.<br /><br />From the photo, I'd say that the GO2/kerosene rocket is not getting a proper mixture or the chamber pressure is way too low. If it were burning correctly, there should be a nice, tight flame and shock diamonds should be visible in the exhaust. Not to be critical, just an observation. Had a similar problem on my initial series of tests due