The Aerodynamics Department is mainly tasked with modeling the aerodynamic forces and analyzing the fluxes generated by our flight systems
The Control Systems Team is an Integrated Project Team (IPT), which is part of the Avionics Department. The members are responsible for the design, implementation and testing of control algorithms that allow the rocket to automatically perform actions
The Electronics IPT (Integrated Project Team), under the more general Avionics Department, is in charge of the design, production and testing of all the on-board and ground electronic systems. These include the rocket’s control software, the telemetry systems, and the data transmission systems
The Logistics Department was established to deal with logistical matters, which include affairs pertaining the procurement of resources and organizational oversight
The Multimedia Communications Department develops and divulges all rocket content to our various media platforms in a passionate and engaging manner
The Mission Analysis IPT is part of the Aerodynamics and Flight Dynamics Department and is responsible for all computational rocket calculations, ranging from the rocket’s trajectory to aerodynamic optimization, and including sensitivity analysis, risk area assessment and engine choice
The propulsion team is in charge of designing, developing, and testing a hybrid rocket engine for participation in EuRoC ‘23 using SRAD thruster
The Recovery Department is responsible for the design, production and testing of all systems tasked with the rocket’s safe return to ground or of some specific part
The Software IPT is a part of the Avionics Department and is in charge of developing both the on-board software and the ground station system which collects and displays the telemetry throughout the mission
The Structures Department is in charge of the entire design and practical implementation of the rocket’s airframe, and is divided in a series of sub-teams, each in charge of a different bay
The Aeroelasticity Analysis IPT was founded in September of 2021 to better study the structural dynamics and the aeroelasticity field of the rocket, as we also improved our knowledge regarding the internal stresses during both the main and drogue parachute opening phases