Spacecraft orbital transfers characterization
Design of a model-rocket with TVC system
Interplanetary and Planetary Mision Analisys
Attitude Dynamics and Control for a 6U CubeSat
Experimental Payload V0
The experimental payload EPv0 is a project of the italian company Sidereus Space Dynamics developed, designed and built with the contribution of PoliSpace. EPv0 aims to characterize through measurements the payload bay of Sidereus’ launcher EOS.
My role inside the team is to help in the design process and in the 3D printing of the components.