| CPC B64C 1/12 (2013.01) [B32B 3/06 (2013.01); B32B 18/00 (2013.01); B64C 1/38 (2013.01); B64C 30/00 (2013.01); C04B 35/565 (2013.01); C04B 35/80 (2013.01); C04B 41/91 (2013.01); C04B 2111/00982 (2013.01); C04B 2237/82 (2013.01)] | 20 Claims |

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1. A skin assembly, comprising:
a first ceramic-matrix-composite skin panel comprising one or more first fingers extending along a first direction; and
a second ceramic-matrix-composite skin panel comprising one or more second fingers extending along the first direction, the one or more second fingers interdigitated with the one or more first fingers to define a plurality of staggered expansion gaps between the first ceramic-matrix-composite skin panel and the second ceramic-matrix-composite skin panel wherein the plurality of staggered expansion gaps are configured to accommodate thermal expansion of at least a portion of the skin assembly when an outer surface of the skin assembly is subject to a speed greater than Mach 5.
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