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A composite barrel assembly for a gun, such as a muzzle-loading mortar for fin-stabilized projectiles. The composite construction of the barrel has a plurality of generally concentric layers built-up around a rigid supporting liner which may be fabricated from any of several metal or ceramic composi

A composite barrel assembly for a gun, such as a muzzle-loading mortar for fin-stabilized projectiles. The composite construction of the barrel has a plurality of generally concentric layers built-up around a rigid supporting liner which may be fabricated from any of several metal or ceramic compositions. An inner thermal barrier coating of inorganic glass, metal refractory alloy, chromium alloy, functionally graded material or ceramic is disposed within the liner. An overwrap layer of continuous fibers embedded in a matrix surrounds the liner. The matrix is either a resin, polymer, ceramic, glass or metal. An outer shell of continuous fibers embedded in a high temperature polymer matrix surrounds the overwrap. When the liner is made from a metal-based composition, an outer thermal barrier coating may be applied in between the liner and the overwrap.

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1. A muzzle-loading mortar assembly for launching a fin-stabilized projectile, said assembly comprising: a barrel having a generally tubular construction centered around a longitudinal axis, said barrel having a breech end and an opposite muzzle end, said barrel having a composite construction compo

1. A muzzle-loading mortar assembly for launching a fin-stabilized projectile, said assembly comprising: a barrel having a generally tubular construction centered around a longitudinal axis, said barrel having a breech end and an opposite muzzle end, said barrel having a composite construction composed of a plurality of generally concentric layers, said plurality of generally concentric layers including a rigid supporting liner having an inner cylindrical surface and an outer surface, aid plurality of generally concentric layers further including an overwrap surrounding said outer surface of said liner and further including an outer thermal barrier disposed between said liner and said overwrap, said outer thermal barrier fabricated from a composition selected from the group consisting essentially of an inorganic glass and a metal refractory alloy and a chromium alloy and a functionally graded material and a ceramic, said liner fabricated from a composition selected from the group consisting essentially of a metal alloy and a metal refractory and a ceramic and a metal matrix composite and a ceramic matrix composite, said liner having an average axial coefficient of thermal expansion, said overwrap comprised of continuous fibers embedded in a matrix, said matrix fabricated from a composition selected from the group consisting essentially of a resin and a polymer and a ceramic and a glass and a metal, said overwrap having an average axial coefficient of thermal expansion approximately matching said average axial coefficient of thermal expansion of said liner, wherein said outer thermal barrier has an average coefficient of thermal expansion that is within a range established between said average axial coefficient of thermal expansion of said liner and said average axial coefficient of thermal expansion of said overwrap. 2. A muzzle-loading mortar assembly for launching a fin-stabilized projectile, said assembly comprising: a barrel having a generally tubular construction centered around a longitudinal axis, said barrel having a breech end and an opposite muzzle end, said barrel having a composite construction composed of a plurality of generally concentric layers, said plurality of generally concentric layers including a rigid supporting liner, said liner having an inner cylindrical surface and an outer surface, wherein said plurality of generally concentric layers comprise an inner thermal barrier disposed within said inner cylindrical surface of said liner, said inner thermal barrier fabricated from a composition selected from the group consisting essentially of an inorganic glass and a metal refractory alloy and a chromium alloy and a functionally graded material and a ceramic, said liner fabricated from a composition selected from the group consisting essentially of a metal alloy and a metal refractory and a ceramic and a metal matrix composite and a ceramic matrix composite, said liner having an average axial coefficient of thermal expansion, said plurality of generally concentric layers including an overwrap surrounding said outer surface of said liner, said overwrap comprised of continuous fibers embedded in a matrix, said matrix fabricated from a composition selected from the group consisting essentially of a resin and a polymer and a ceramic and a glass and a metal, said overwrap having an average axial coefficient of thermal expansion approximately matching said average axial coefficient of thermal expansion of said liner, wherein said inner thermal barrier has an average coefficient of thermal expansion that is within a range established between said average axial coefficient of thermal expansion of said liner and said average axial coefficient of thermal expansion of said overwrap. 3. A muzzle-loading mortar assembly for launching a fin-stabilized projectile, said assembly comprising: a barrel having a generally tubular construction centered around a longitudinal axis, said barrel having a breech end and an opposite muzzle end, said barrel having a composite construction composed of a plurality of generally concentric layers, said plurality of generally concentric layers including a rigid supporting liner, said liner fabricated from a composition selected from the group consisting essentially of a metal alloy and a metal refractory and a ceramic and a metal matrix composite and a ceramic matrix composite, said liner having an inner cylindrical surface and an outer surface, said liner having an average axial coefficient of thermal expansion, said plurality of generally concentric layers including an overwrap surrounding said outer surface of said liner, said overwrap comprised of continuous fibers embedded in a matrix, wherein said continuous fibers of said overwrap are fabricated from a composition selected from the group consisting essentially of carbon fibers and boron fibers and silicon carbide fibers, wherein said continuous fibers are laid-up around said liner in a plurality of layers and at a plurality of winding angles relative to said longitudinal axis, wherein at least one layer of said plurality of layers has a dissimilar radial thickness relative to at least one other layer of said plurality of layers, said matrix fabricated from a composition selected from the group consisting essentially of a resin and a polymer and a ceramic and a glass and a metal, said overwrap having an average axial coefficient of thermal expansion approximately matching said average axial coefficient of thermal expansion of said liner, and wherein at least one layer of said plurality of layers comprises a dissimilar fiber composition relative to at least one other layer of said plurality of layers. 4. A muzzle-loading mortar assembly for launching a fin-stabilized projectile, said assembly comprising: a barrel having a generally tubular construction centered around a longitudinal axis, said barrel having a breech end and an opposite muzzle end, said barrel having a composite construction composed of a plurality of generally concentric layers, said plurality of generally concentric layers including a rigid supporting liner, said liner fabricated from a composition selected from the group consisting essentially of a metal alloy and a metal refractory and a ceramic and a metal matrix composite and a ceramic matrix composite, said liner having an inner cylindrical surface and an outer surface, said liner having an average axial coefficient of thermal expansion, said plurality of generally concentric layers including an overwrap surrounding said outer surface of said liner, said overwrap comprised of continuous fibers embedded in a matrix, wherein said continuous fibers of said overwrap are fabricated from a composition selected from the group consisting essentially of carbon fibers and boron fibers and silicon carbide fibers, wherein said continuous fibers are laid-up around said liner in a plurality of layers and at a plurality of winding angles relative to said longitudinal axis, said matrix fabricated from a composition selected from the group consisting essentially of a resin and a polymer and a ceramic and a glass and a metal, said overwrap having an average axial coefficient of thermal expansion approximately matching said average axial coefficient of thermal expansion of said liner, wherein at least one layer of said plurality of layers comprises a dissimilar fiber wrap angle relative to at least one other layer of said plurality of layers. 5. A muzzle-loading mortar assembly for launching a fin-stabilized projectile, said assembly comprising: a barrel having a generally tubular construction centered around a longitudinal axis, said barrel having a breech end and an opposite muzzle end, said barrel having a composite construction composed of a plurality of generally concentric layers, said plurality of generally concentric layers including a rigid supporting liner, said liner fabricated from a composition selected from the group consisting essentially of a metal alloy and a metal refractory and a ceramic and a metal matrix composite and a ceramic matrix composite, said liner having an inner cylindrical surface and an outer surface, said liner having an average axial coefficient of thermal expansion, said plurality of generally concentric layers including an overwrap surrounding said outer surface of said liner, said overwrap comprised of continuous fibers embedded in a matrix, wherein said continuous fibers of said overwrap are fabricated from a composition selected from the group consisting essentially of carbon fibers and boron fibers and silicon carbide fibers, wherein said continuous fibers are laid-up around said liner in a plurality of layers and at a plurality of winding angles relative to said longitudinal axis, said matrix fabricated from a composition selected from the group consisting essentially of a resin and a polymer and a ceramic and a glass and a metal, said overwrap having an average axial coefficient of thermal expansion approximately matching said average axial coefficient of thermal expansion of said liner, wherein at least one layer of said plurality of layers comprises a dissimilar fiber tension relative to at least one other layer of said plurality of layers. 6. A muzzle-loading mortar assembly for launching a fin-stabilized projectile, said assembly comprising: a barrel having a generally tubular construction centered around a longitudinal axis, said barrel having a breech end and an opposite muzzle end, said barrel having a composite construction composed of a plurality of generally concentric layers, said plurality of generally concentric layers including a rigid supporting liner, said liner fabricated from a composition selected from the group consisting essentially of a metal alloy and a metal refractory and a ceramic and a metal matrix composite and a ceramic matrix composite, said liner having an inner cylindrical surface and an outer surface, said liner having an average axial coefficient of thermal expansion, said plurality of generally concentric layers including an overwrap surrounding said outer surface of said liner, said overwrap comprised of continuous fibers embedded in a matrix, said matrix fabricated from a composition selected from the group consisting essentially of a resin and a polymer and a ceramic and a glass and a metal, said overwrap having an average axial coefficient of thermal expansion approximately matching said average axial coefficient of thermal expansion of said liner, wherein said plurality of generally concentric layers includes an outer shell surrounding said overwrap, said outer shell comprised of continuous fibers embedded in a thermoset polymerizable monomer reactant (PMR) polyimide resin matrix. 7. A composite barrel assembly for a gun that launches projectiles driven by the action of an explosive force, said assembly comprising: a barrel having a generally tubular construction centered around a longitudinal axis, said barrel having a breech end and an opposite muzzle end, said barrel having a composite construction composed of a plurality of generally concentric layers,said plurality of generally concentric layers including a rigid supporting liner, said liner fabricated from a composition selected from the group consisting essentially of a metal alloy and a metal refractory and a ceramic and a metal matrix composite and a ceramic matrix composite, said liner having an inner cylindrical surface and an outer surface, said plurality of generally concentric layers including an overwrap surrounding said outer surface of said liner, said overwrap comprised of continuous fibers embedded in a matrix, said matrix fabricated from a composition selected from the group consisting essentially of a resin and a polymer and a ceramic and a glass and a metal,said plurality of generally concentric layers including an inner thermal barrier disposed within said inner cylindrical surface of said liner, said inner thermal barrier fabricated from a composition selected from the group consisting essentially of an inorganic glass and a metal refractory alloy and a chromium alloy and a functionally graded material and a ceramic,said plurality of generally concentric layers including an outer shell surrounding said overwrap, said outer shell comprised of continuous fibers embedded in a thermoset PMR polyimide resin matrix, wherein said liner has an average axial coefficient of thermal expansion, said overwrap having an average axial coefficient of thermal expansion approximately matching said average axial coefficient of thermal expansion of said liner, wherein said inner thermal barrier is fabricated from a composition selected from the group consisting essentially of an inorganic glass and a metal refractory alloy and a chromium alloy and a functionally graded material and a ceramic, said inner thermal barrier having an average coefficient of thermal expansion that is within a range established between said average axial coefficient of thermal expansion of said liner and said average axial coefficient of thermal expansion of said overwrap. 8. A muzzle-loading mortar assembly for launching a fin-stabilized projectile, said assembly comprising: a barrel having a generally tubular construction centered around a longitudinal axis, said barrel having a breech end and an opposite muzzle end, a blast attenuator affixed to said muzzle end, said breech end being closed, said barrel having a composite construction composed of a plurality of generally concentric layers, said plurality of generally concentric layers including a rigid supporting liner, said liner fabricated from a composition selected from the group consisting essentially of a metal alloy and a metal refractory and a ceramic and a metal matrix composite and a ceramic matrix composite, said liner having an average axial coefficient of thermal expansion, said liner having an inner cylindrical surface and an outer surface, said plurality of generally concentric layers including an inner thermal barrier disposed within said inner cylindrical surface of said liner, said inner thermal barrier having an average coefficient of thermal expansion, said inner thermal barrier fabricated from a composition selected from the group consisting essentially of an inorganic glass and a metal refractory alloy and a chromium alloy and a functionally graded material and a ceramic, said inner thermal barrier including fiber reinforcement, said plurality of generally concentric layers including an outer thermal barrier surrounding said liner, said outer thermal barrier fabricated from a composition selected from the group consisting essentially of an inorganic glass and a metal refractory alloy and a chromium alloy and a functionally graded material and a ceramic, said outer thermal barrier having an average coefficient of thermal expansion, said outer thermal barrier including fiber reinforcement, said plurality of generally concentric layers including an overwrap surrounding said outer thermal barrier, said overwrap comprised of continuous fibers embedded in a matrix, said overwrap having an average axial coefficient of thermal expansion approximately matching said average coefficient of thermal expansion of said liner, said continuous fibers fabricated from a composition selected from the group consisting essentially of carbon fibers and boron fibers and silicon carbide fibers, said continuous fibers being wound around said liner in a plurality of layers and at a plurality of winding angles relative to said longitudinal axis, at least one layer of said plurality of layers having a dissimilar radial thickness relative to at least one other layer of said plurality of layers, at least one layer of said plurality of layers comprising a dissimilar fiber composition relative to at least one other layer of said plurality of layers, at least one layer of said plurality of layers comprising a dissimilar fiber wrap angle relative to at least one other layer of said plurality of layers, at least one layer of said plurality of layers comprising a dissimilar fiber tension relative to at least one other layer of said plurality of layers, said matrix fabricated from a composition selected from the group consisting essentially of a resin and a polymer and a ceramic and a glass and a metal, said plurality of generally concentric layers including an outer shell surrounding said overwrap, said outer shell comprised of continuous fibers embedded in a thermoset PMR polyimide resin matrix, wherein said average coefficient of thermal expansion of said inner thermal barrier is within a range established between said average axial coefficient of thermal expansion of said liner and said average axial coefficient of thermal expansion of said overwrap, wherein said average coefficient of thermal expansion of said outer thermal barrier is within a range established between said average axial coefficient of thermal expansion of said liner and said average axial coefficient of thermal expansion of said overwrap,a baseplate, a coupling interconnecting said baseplate and said breech end of said barrel for articulating movement therebetween, said baseplate having a plurality of cleats,a mounting arm connected to said barrel, said mounting arm including a length adjustment device, said mounting arm including an angular adjustment device, anda sighting unit affixed relative to said barrel for optically surveying a downrange target.