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A shield for use with a detector includes a first opening adjacent the detector, a second opening opposite the first opening along an optical axis intersecting the detector, and a field of view defined by the detector and the second opening. A shield body includes alternating curved profile regions

A shield for use with a detector includes a first opening adjacent the detector, a second opening opposite the first opening along an optical axis intersecting the detector, and a field of view defined by the detector and the second opening. A shield body includes alternating curved profile regions and linear profile regions coaxially aligned along the optical axis. The curved profile regions have respective curved interior surfaces concave facing toward the second opening, and the linear profile regions have respective interior surfaces facing toward the first opening. In this way, specular reflections associated with stray light may be greatly reduced.

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1. A shield for use with a detector, the shield comprising: a first opening adjacent the detector;a second opening opposite the first opening along an optical axis intersecting the detector, wherein a field of view is defined by the detector and the second opening;a shield body comprising alternatin

1. A shield for use with a detector, the shield comprising: a first opening adjacent the detector;a second opening opposite the first opening along an optical axis intersecting the detector, wherein a field of view is defined by the detector and the second opening;a shield body comprising alternating curved profile regions and linear profile regions coaxially aligned along the optical axis;wherein the curved profile regions have respective curved interior surfaces concave facing toward the second opening; andwherein the linear profile regions have respective interior surfaces facing toward the first opening. 2. The shield of claim 1, wherein the curved profile regions are solids of revolution defined by an arc rotated about an arbitrary shape enclosing the optical axis. 3. The shield of claim 1, wherein the linear profile regions an solids of revolution defined by a line segment rotated about an arbitrary shape enclosing the optical axis. 4. The shield of claim 1, wherein: the shield body includes n curved profile regions;the first curved profile region is adjacent the first opening; andthe nth curved profile region is adjacent the second opening. 5. The shield of claim 4, wherein n is greater than two. 6. The shield of claim 4, wherein n is geometrically defined by the field of view and an allocated volume for the shield. 7. The shield of claim 6, wherein each curved profile region intersects an adjacent linear profile region at an edge substantially located along the field of view. 8. The shield of claim 7, wherein the edge has a radius of curvature less than approximately 0.002 inches. 9. The shield of claim 7, wherein the linear profile regions are defined by line segments collinear with a reference point adjacent the second opening at an opposite side of the second opening. 10. The shield of claim 1, wherein the shield body is a thin-walled structure having a thermal conductivity greater than about 200 W/m-K. 11. The shield of claim 10, wherein the shield body comprises beryllium. 12. The shield of claim 10, wherein the shield body comprises a radiation-shielding material. 13. The shield of claim 10, wherein the thin-walled structure has a thickness of less than approximately 0.005 inches. 14. The shield of claim 1, further comprising a low-emissivity black coating on the interior surfaces. 15. A method of manufacturing a cold shield for use with a detector having an allocated volume, a field of view, and an optical axis, the method comprising: forming a monolithic shield body;forming, within the monolithic shield body, a first opening and a second opening opposite the first opening along the optical axis; andforming, within the monolithic shield body, alternating curved profile regions and linear profile regions coaxially aligned along the optical axis such that the curved profile regions have respective curved interior surfaces concave facing toward the second opening and the linear profile regions have respective interior surfaces facing toward the first opening. 16. The method of claim 15, further including manufacturing the shield body such that each curved profile region intersects an adjacent linear profile region at an edge substantially located along the field of view. 17. The method of claim 15, wherein manufacturing the shield body includes spray-forming the shield body. 18. The method of claim 17, wherein the spray-forming includes spray-forming a beryllium-bearing material. 19. A missile assembly comprising: a missile body;a detector coupled to the missile body and configured to detect infrared radiation within a field of view external to the missile along an optical axis;a cold shield having a first opening adjacent the detector, a second opening opposite the first opening along the optical axis, and a shield body comprising alternating curved profile regions and linear profile regions coaxially aligned along the optical axis;wherein the curved profile regions have respective curved interior surfaces concave facing toward the second opening;wherein the linear profile regions have respective interior surfaces facing toward the first opening; andwherein the shield body is geometrically defined by the field of view and a predetermined allocated volume for the shield body. 20. The missile assembly of claim 19, wherein each curved profile region intersects an adjacent linear profile region at an edge substantially located along the field of view, and wherein the linear profile regions are defined by line segments collinear with a reference point adjacent the second opening on an opposite side of the opening.