Project Vulcan
Dates: 2024 June - Current
A Bi-propellant rocket engine that runs on Gaseous Oxygen and Ethanol. I wrote a research paper on its design, and am writing another one about the impact of changing nozzles on engine efficiency, with a focus on aerospike nozzles. The Github holds the control system code and details, the document is my research paper, I've also linked my youtube channel!