Conceptual Shaft System Design
Mars Rover Transmission Shaft
This project develops a shaft-system concept for a Martian drilling application. Instead of treating the shaft as a single sizing exercise, the work breaks the problem into symbolic layout, reaction-force analysis, bending and torsion interpretation, equivalent moment calculations, and final material-informed diameter decisions.
Project Overview
The work starts with a functional transmission requirement for Martian drilling and then moves into the classical machine-design questions that make the concept useful: where are the loads, how do they combine, and what does that mean for geometry and material choice?
Design Method
I built the logic through free-body thinking first and then into force, shear, moment, and equivalent bending diagrams. That makes the final shaft sizing easier to trust because the intermediate steps remain visible.
Material Choice
The final presentation selects 42CrMo4 (AISI 4140), which fits the need for high strength and fatigue resistance in a system expected to handle dynamic and shock loading.
Key Results
Final shaft diameters were derived from equivalent bending moment analysis combining torsion and bending loads. The output shaft required larger cross-sections at the gear interface due to higher combined loading at that station.
Mechanical Breakdown
From symbolic layout to final shaft sizing.