In selecting a starter motor for a gas turbine, it is crucial to determine whether the minimum torque or inertia needed to overcome is that of the compressor, the turbine, or both. The gearbox is essential for initiating the engine start by spinning the shaft, which also requires consideration of the torque needed to move air through the blades. Initially, the starter motor primarily assists the compressor, as it must be operational to facilitate combustion. Once the combustion process begins and the turbine starts moving, it then drives the compressor, making the system self-sustaining. The discussion highlights the complexities and interdependencies in gas turbine design, often laced with sarcasm regarding the perceived simplicity of jet engine engineering.