Orion Launch Today
Discussion
i guess they are going for a "steep" high G force entry to try to simulate the typical energies involved with coming back from non earth orbital paths (ie deep space). The requirements for a heat shield are very different, as you need to balance both peak thermal loading with total energy rejection. ie, you can have a thick low grade heat shield that can reject a lower temperature for a longer time (think space shuttle) or a thin high grade one which can resist a much higher temp, but for not as long. Steep entries with large decelerations mean you reach a denser atmosphere at a high speed, rather than spend longer losing your speed at a higher altitude. As such, peak heating is later in the descent profile, and also gives things like your arrester systems the greatest work out etc.
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