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The first image shows the global heating data acquired on the windward surface of the vehicle during a continuous pitch sweep with both inlets started. In the second image the color changes represent the global heating data acquired on the windward surface of the vehicle during a continuous pitch sweep with the starboard inlet unstarted.


AEDC and AFRL collaborate to make advances in hypersonic technology

The first image shows the global heating data acquired on the windward surface of the vehicle during a continuous pitch sweep with both inlets started. In the second image the color changes represent the global heating data acquired on the windward surface of the vehicle during a continuous pitch sweep with the starboard inlet unstarted.

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