Our team is composed undergraduate students from multiple disciplines across campus and divided into 5 departments: Engine Development, Propellant Systems, Test Stand, Automation Systems and Business Development. The engine is designed with a 1.3 mixture ratio (O/F) of Jet Fuel-A and Gaseous Oxygen (GOX), to produce 50 lbf (222N) of thrust at sea level with a chamber pressure of 60 psig (413.7 kPa).
Founded in 2019, the engine has undergone multiple iterations, presented on the right, with the latest design being established in 2022. This last design incorporates a coaxial swirl injector made of brass, and ablative materials for the internal geometry. The team is currently prototyping and cold flow testing the injector manifold assembly to validate the design and performance, as well as practice and troubleshoot the pipe routing and sensors that will eventually be implemented in hot fire test.