Our Thermal Team’s main goal is to design and fabricate the main engine, fuel injection, and ignition systems.

Currently, we are utilizing programs like Rocket Propulsion Analysis (RPAv4) to gather data and assist in the design of our nozzle and chamber geometry.

In addition, we are actively working on modeling said geometry through the use of Dassault Systèmes SOLIDWORKS to produce 3D CAD models which can be further used to virtually assemble our project as well as applied to other simulation programs.