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Methods and compositions for fabricating composite parts including at least one structural material and at least one protective material that are integrally bonded without the use of secondary bonding operations. One or more of the materials forming the layers of the composite parts may be a ceramic

Methods and compositions for fabricating composite parts including at least one structural material and at least one protective material that are integrally bonded without the use of secondary bonding operations. One or more of the materials forming the layers of the composite parts may be a ceramic composition with or without porosity and one or more of the materials may be a polymer composition. Methods including co-injection processes also are provided for fabricating multi-layered structures in which each layer serves a desired function while still being integrated into the overall structure.

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1. A co-cured non-metallic composite part for use in environments having elevated temperatures comprising a plurality of layers of non-metallic materials, said layers including:a first layer of a first non-metallic substrate material for providing structural support for the composite part; anda seco

1. A co-cured non-metallic composite part for use in environments having elevated temperatures comprising a plurality of layers of non-metallic materials, said layers including:a first layer of a first non-metallic substrate material for providing structural support for the composite part; anda second layer of a second non-metallic material overlaying the first layer, said second material characterized by limiting the effects of heat on the first layer, the second material formed from a ceramic composition, the second material having a porosity of at least about 20 percent by volume;the co-cured composite part having no metallic substrate and having improved bonding of the first and second layers and reduced occurrence of delamination of the first and second layers as compared to a composite part of mechanically joined layers.2. The composite part of claim 1 wherein the first material is a polymer composite composition.3. The composite part of claim 2 wherein the polymer composite composition is selected from the group consisting of fiberglass, vinyl ester, epoxy and mixtures thereof.4. The composite part of claim 2 wherein the first material includes a reinforcement material.5. The composite part of claim 1 wherein the ceramic composition has a thermal conductivity of no more than about 10 W/mK.6. The composite part of claim 1 wherein both the first and the second materials are a ceramic composition.7. The composite part of claim 1, wherein the composite put includes a separation layer between the first and second layer for maintaining the first layer in generally spaced relation with the second layer during fabrication.8. The composite part of claim 1 wherein the second material includes internal pores having diameters between about 50 to about 100 μm.9. The composite part of claim 1 wherein the second layer is of a material and having a thickness effective for protecting the composite part from the effects of temperatures of at least about 1200° C.10. The composite part of claim 7 wherein the separation layer is compatible with but generally permeable to the first and second materials to allow chemical and mechanical bonding of the materials.11. The composite part of claim 10, wherein the separation layer includes a thermoplastic film, a thermoset film adhesive and combinations thereof.12. The composite part of claim 1 further comprising a third non-metallic layer, wherein the second layer is adjacent one surface of the first layer and the third layer is adjacent a surface of the first layer opposite the one surface and wherein the third layer limits the effects of heat on the first layer.13. The composite part of claim 1 wherein the second material has a porosity of between about 20 to about 60 percent by volume.14. A non-metallic missile system component part comprising a non-metallic structural support layer and one or more non-metallic heat insulating layers formed from one or more ceramic compositions having a porosity of at least about 20 percent by volume and adjacent one or more outer surfaces of the structural support layer, wherein the component part does not include a metallic substrate and wherein the layers of the component part are integrally fabricated to provide improved bonding and limit delamination of the layers as compared to a component part having layers that are mechanically secured.15. The component part of claim 14 wherein the structural support layer is a polymer composition.16. The component part of claim 15 wherein the polymer composition includes a reinforcement material.17. The component part of claim 14 wherein the ceramic composition includes a reinforcement material and has a porosity of between about 20 to about 50 percent.18. The component part of claim 14 wherein the structural support layer is a ceramic composition.19. The component part of claim 18 wherein the ceramic composition includes a reinforcement material.20. The composite part of claim 14 wherein the ceramic composition has a dielectric constant effective for radar absorption.