Static Engine Fire

In this test, we will run ethanol pressurized with nitrogen gas through our ethanol tower and nitrous oxide through our nitrous tower and feed these into the injector and into the combustion chamber, where they will ignite and go through the nozzle to get a reading on the thrust. This test has particular emphasis on ignition, injector functionality, and hazard prevention since it models what our actual rocket's interior will consist of.

More information soon to come!