Our team is composed of undergraduate students from multiple disciplines across campus and is divided into five 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. The latest 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 to practice and troubleshoot the pipe routing and sensors that will eventually be implemented in hot fire test.
About Us
What's expected
We have recently started our vehicle integration campaign and are undergoing extensive research to create our first fully reusable liquid rocket engine. This campaign is now being run alongside our liquid propulsion rocket engine that will be undergoing its first Hot-Fire Test by early march.
Version 3
2021
Version 4
2022
Version 5
2024
Version 2
2020
Version 1
2019























