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Separation Dynamics of Spinning Spacecraft and Deployment Arm Requirements.

Spring 2024

For my master’s design project, I developed a MATLAB/Simulink script to model the separation dynamics of a spinning ride-share spacecraft. This involved simulating potential missions using existing orbital data to validate the efficacy of the technology. Based on the results of the simulations and analysis, I drafted design requirements to guide further development of the deployment arm and the Mailboy spacecraft.

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