Four aircraft are tasked to track Orion across 1,701 nautical miles of descent at Mach 32, collecting real-time heating data through telescopes and sensors. The aerial relay reflects the limits of ground-based re-entry simulation at lunar-return velocities. No wind tunnel or computational model fully reproduces the coupled plasma, ablation, and gas dynamics of a crewed capsule at Mach 32. This is the same modelling gap that caused NASA to miss both the char loss and the bolt erosion on Artemis I. The relay exists because NASA needs empirical data.
The separately recovered external sensor adds a second data stream: measurements taken from outside the capsule's ablative boundary layer, which cannot be replicated by internal instrumentation alone.
