Dynamic thermal simulation of a reusable inflatable atmospheric decelerator during entry and descent from LEO towards Earth

Packard C, Pradhani N, di Bari G, Blazejewski Z, Canull L, Haidar F

Presents dynamic thermal simulation results for a reusable inflatable atmospheric decelerator during atmospheric entry and descent from low Earth orbit, using MuSES to evaluate heating environments and structural thermal performance.

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