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.
