You will evaluate complex engineering tradeoffs involving structural performance, manufacturability, thermal interfaces, assembly, transportation, testing, launch vehicle integration, and on-orbit operations to ensure the spacecraft performs as an optimized system rather than a collection of individual subsystems. Working across Mechanical, Electrical, Thermal, RF, Propulsion, Manufacturing, Test, and Systems Engineering, you will develop structural solutions that integrate every subsystem into a cohesive, manufacturable, and flight-ready vehicle.