As a member of the Raven Alumni program, I continue my collaboration with the project as a counsellor and adjunct help for the progression of the project. In exchange for my knowledge of the initial stages of development and partial availability, I will maintain access to the documentation and evolution of the organization itself.

Developed "Verification and Testing plan" for the entire propulsive subsystem.Preliminary Design Presentation and review with industry experts. Redesigned of the subsystem to increase ease of manufacture and performance. Evaluated temperature in the nozzle material throughout the duration of the burn time via transient thermal simulations.

Studied the implementation of a Pre-combustion chamber and a Post-combustion chamber for a Hybrid rocket. Developed a modular MATLAB algorithm that allows isentropic flow evaluation and engine performance calculations. Determined best possible supersonic area ratio and shape for low altitude nozzle.Nozzle material selection aided by simulation of the interaction between flow and walls.

As a board member, I participate actively in all GSO meetings concerning various topics, such as member allocations, recruitment procedures, project interactions and founding.As Project RAVEN representative in GSO, I update the rest of the board on the status of the project as well as bring up talking points from and to it, trying to highlight its interests.

The rapidly expanding research on Metal Combustion as a reliable and renewable energy carrier has an incredibly high potential for Space technologies. In this thesis, Metal combustion will be applied to the field of Space Propulsion, with a particular focus on lunar missions.https://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-94148

Developed the platform for a constellation of telecommunications satellites in Very Low Earth Orbit (VLEO). As a member of the Mechanics team, I developed the satellite's structures, and mechanisms, as well as the thermal control system and general architecture of the satellite. I was in charge of the propulsion system of the satellite which uses the innovative Air-Breathing Electric Propulsion (ABEP) technology that gives longevity and competitiveness to the constellation. Finally, I was responsible for developing the deployment and release system for 100 satellites per launch, considering several launchers available on the market.