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We used ANSYS and Creo to carry out our lander model Simulation. The base model was created in Creo and then exported to Ansys for further analysis. The simulation results were compared with actual prototyping results to gain better understanding of our design. 

Subsystem tests were performed to help make key design decisions. The first test helped in determining the optimal shape of the crushable bottom. More sub-system tests may be added in future design and prototype iterations. Tests:

This subsystem test helped in determining the best orientation of the crushable bottom. The honeycomb can be in a vertical or horizontal direction which changes how much it crushes. Therefore, the honeycomb crushable bottom was tested in both orientations to determine which can endure higher forces and energy impact. 

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