spenvis

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annie-schofield / Spacecraft-Design-for-Jovian-Missions

High-fidelity simulation of a Ganymede polar orbiter using TudatPy to model multi-body gravity and radiation pressure. Integrated with SPENVIS/JOSE to characterize the Jovian electron radiation environment and calculate the optimal aluminum shielding thickness required for mission survival.

spacecraft-trajectories radiation-physics jovian tudat spacecraft-design spenvis

Updated Feb 3, 2026
Python

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spenvis

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annie-schofield / Spacecraft-Design-for-Jovian-Missions

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