Hybrid composite articles and missile components, and their...

Details Hybrid composite articles and missile components, and their... Hybrid composite articles and missile components, and their...

B - Operations, Transporting

32

B

B32B 15/14 (2006.01) F42B 12/76 (2006.01)

Patent

CA 2177216

A surface-protected composite article (40), such as a component of a missile (20), is prepared with a heat-sink substrate (42), a first composite layer (44) of an pre-ceramic-matrix structural composite material, and a second composite layer (46) of a reinforced silicone pre-ceramic material. The siliconematerial is co-curable with the organic matrix of the first composite layer (44). The silicone at the surface (48) of the article (40) is thereafter converted to a silica refractory by an appropriate treatment such as exposure to an oxygen-richplasma or a high-surface temperature. The silica protects the surface of the composite material.

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