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A structural composite laminate and method of making the same are provided. The laminate includes first and second skins or laminas, and a core positioned between the first and second laminas. The core contains thermoplastic and/or substantially inelastic polymeric particles with inter-particle inte

A structural composite laminate and method of making the same are provided. The laminate includes first and second skins or laminas, and a core positioned between the first and second laminas. The core contains thermoplastic and/or substantially inelastic polymeric particles with inter-particle interstices between the polymeric particles. Optionally, the polymeric particles are arranged discontinuously to establish gaps between adjacent particles along at least one dimension of the laminate.

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1. A process for making a structural composite laminate, comprising: providing a first lamina;depositing a plurality of solid yet deformable discrete, non-porous, thermoplastic polymeric particles having surfaces on the first lamina to establish a core, wherein inter-particle voids extend surface to

1. A process for making a structural composite laminate, comprising: providing a first lamina;depositing a plurality of solid yet deformable discrete, non-porous, thermoplastic polymeric particles having surfaces on the first lamina to establish a core, wherein inter-particle voids extend surface to surface from and to the respective surfaces of adjacent thermoplastic polymeric particles;applying a second lamina over the core;applying a sufficient compressive force to the first and second laminas to permanently deform the thermoplastic polymeric particles into a deformed state between the first and second laminas while retaining the inter-particle voids and maintaining the thermoplastic polymeric particles as non-porous; andreleasing the compressive force without delaminating the first and second laminas from the thermoplastic polymeric particles to thereby provide a structural composite laminate comprising the first lamina, the second lamina, and a core between the first and second laminas the core comprising the non-porous thermoplastic polymeric particles substantially retained in the deformed state and having the inter-particle voids. 2. The process of claim 1, wherein said applying a sufficient compressive force comprises moving the first and second laminas towards one another at an effective temperature to permanently deform the thermoplastic polymeric particles into the deformed state. 3. The process of claim 1, wherein the first and second laminas comprise metals. 4. The process of claim 1, wherein the core possesses a monolayer of the thermoplastic polymeric particles. 5. The process of claim 1, wherein the core possesses a plurality of layers of the thermoplastic polymeric particles stacked one on top of another. 6. The process of claim 1, further comprising: applying a first adhesive to join the first lamina to the core; andapplying a second adhesive to join the second lamina to the core. 7. The process of claim 1, wherein the thermoplastic polymeric particles comprise copolymers thermally bonding the first and second outer layers to one another free of a separate adhesive layer. 8. The process of claim 1, wherein the thermoplastic polymeric particles are arranged discontinuously from one another along at least one dimension of the laminate. 9. The process of claim 1, wherein the thermoplastic polymeric particles have a compression set greater than 30 percent as measured by ASTM D395 at 50° C. for 24 hours. 10. A process for making a structural composite laminate, comprising: providing a first lamina;depositing a plurality of solid yet deformable discrete, non-porous, substantially inelastic polymeric particles having surfaces on the first lamina to establish a core, wherein inter-particle voids extend surface to surface from and to the respective surfaces of adjacent substantially inelastic polymeric particles;applying a second lamina over the core;applying a sufficient compressive force to the first and second laminas to permanently deform the substantially inelastic polymeric particles into a deformed state between the first and second laminas while retaining the inter-particle voids and maintaining the polymeric particles as non-porous; andreleasing the compressive force without delaminating the first and second laminas from the substantially inelastic polymeric particles to thereby provide a structural composite laminate comprising the first lamina, the second lamina, and a core between the first and second laminas, the core comprising the non-porous, substantially inelastic polymeric particles substantially retained in the deformed state and having the inter-particle voids. 11. The process of claim 10, wherein said applying a sufficient compressive force comprises moving the first and second laminas towards one another at an effective temperature to permanently deform the substantially inelastic polymeric particles into the deformed state. 12. The process of claim 10, wherein the substantially inelastic polymeric particles have a compression set greater than 30 percent as measured by ASTM D395 at 50° C. for 24 hours. 13. The process of claim 10, wherein the first and second laminas comprise metals. 14. The process of claim 10, wherein the core possesses a monolayer of the substantially inelastic polymeric particles. 15. The process of claim 10, wherein the core possesses a plurality of layers of the substantially inelastic polymeric particles stacked one on top of another. 16. The process of claim 10, further comprising: applying a first adhesive to join the first lamina to the core; andapplying a second adhesive to join the second lamina to the core. 17. The process of claim 10, wherein the substantially inelastic polymeric particles comprise copolymers thermally bonding the first and second outer layers to one another free of a separate adhesive layer. 18. The process of claim 10, wherein the substantially inelastic polymeric particles are arranged discontinuously from one another along at least one dimension of the laminate. 19. A process for making a structural composite laminate, comprising: applying a compression force to a plurality of solid yet deformable discrete, non-porous, substantially inelastic polymeric particles situated between first and second lamina to deform the polymeric particles into a deformed state, and releasing the compression force without delaminating the first and second lamina from the substantial inelastic polymeric particles to form a structural composite laminate, the structural composite laminate comprising the first and second lamina bonded to the non-porous, substantially inelastic polymeric particles substantially retained in the deformed state with inter-particle voids extending surface to surface from and to respective surfaces of adjacent particles of the non-porous, substantially inelastic polymeric particles. 20. The process of claim 19, further comprising heating the substantially inelastic polymeric particles to at least partially melt the particles. 21. The process of claim 19, further comprising heating the substantially inelastic polymeric particles to fuse the particles to one another. 22. The process of claim 19, wherein the substantially inelastic polymeric particles are arranged discontinuously with respect to one another. 23. The process of claim 19, wherein the substantially inelastic polymeric particles are arranged in continuous contact with one another. 24. The process of claim 19, wherein said applying the compressive force comprises moving the first and second laminas towards one another to deform the polymeric particles. 25. The process of claim 24, further comprising heating the first and second lamina to heat the polymeric particles.