Patent Number: 
Section: claims

1. A cooling system for an extreme ultraviolet (EUV) grazing incidence collector (GIC) having at least one shell with a back surface and a central axis, comprising:a plurality of spaced apart substantially circular cooling lines arranged in substantially parallel planes that are substantially perpendicular to the shell central axis, the cooling lines thermally contacting and running around a corresponding circumference of the back surface; andinput and output cooling-fluid manifolds respectively fluidly connected to the plurality of cooling lines at spaced apart input and output locations to flow a cooling fluid from the input cooling-fluid manifold to the output cooling-fluid manifold over two paths for each cooling line. 2. The cooling system of claim 1, wherein the spaced apart input and output locations are arranged substantially 180° apart so that the two paths for each cooling line are substantially semicircular. 3. The system of claim 1, including a conformal metal layer that covers the shell back surface and at least a portion of the plurality of cooling lines. 4. The system of claim 3, wherein the at least one shell is electroformed, and wherein the conformal metal layer comprises an electroformed layer. 5. The system of claim 1, wherein the at least one shell comprises an electroformed metal or metal alloy, and the plurality of cooling lines comprise said metal or metal alloy. 6. The system of claim 1, wherein the plurality of cooling lines have more than one cooling line diameter. 7. The system of claim 1, wherein at least one pair of adjacent cooling lines have an outside diameter DO and are spaced apart from one another by at least one of:a) a center-to-center distance of at least about 3×DO; andb) a edge-to-edge distance of at least about 2×DO. 8. The system of claim 1, wherein at least one pair of adjacent cooling lines have an outside diameter DO and are spaced apart from one another by at least one of:a) a center-to-center distance of at least about 2×DO; andb) a edge-to-edge distance of at least about 1×DO. 9. The system of claim 1, wherein at least some of the cooling lines have a non-circular cross-section. 10. The system of claim 1, further comprising a flow-control device adapted to control the flow of cooling fluid through a corresponding cooling line. 11. The system of claim 1, wherein the shell has an edge, and wherein a cooling line is arranged immediately adjacent the edge but without shadowing EUV radiation when the shell is operably arranged relative to an EUV radiation source. 12. The system of claim 1, wherein the edge cooling line has a non-circular cross-section. 13. The cooling system of claim 1, further comprising alloy-brazed connections that fluidly connect the plurality of cooling lines and the input and output cooling-fluid manifolds. 14. The system of claim 1, further comprising:a plurality of spaced-apart nested shells each having respective pluralities of cooling lines connected to the input and output cooling-fluid manifolds; anda stand-off device configured to maintain the spaced-apart configuration of the nested shells. 15. The system of claim 1, further comprising:input and output main cooling-fluid manifolds; andinput and output feeder lines that respectively connect the input and output cooling-fluid manifolds to the input and output main cooling-fluid manifolds. 16. The system of claim 1, wherein the input and output cooling-fluid manifolds are configured to control a rate of cooling fluid flow to control a temperature difference between the input and output locations of the plurality of cooling lines. 17. The system of claim 1, wherein the GIC shell includes first and second segments that respectively receive first and second thermal loads from an EUV light source, and wherein the cooling lines on the first and second segment are configured to provide respective first and second amounts of thermal cooling corresponding to the first and second thermal loads. 18. The system of claim 17, wherein the cooling lines on the first and second segments are configured to provide varying amounts of thermal cooling corresponding to a variation in thermal load over the respective segments. 19. An extreme ultraviolet (EUV) lithography system for illuminating a reflective mask, comprising:a source of EUV radiation;a GIC collector having the cooling system of claim 1 and configured to receive the EUV radiation and form collected EUV radiation; andan illuminator configured to receive the collected EUV radiation and form condensed EUV radiation for illuminating the reflective reticle. 20. The EUV lithography system of claim 19 for forming a patterned image on a photosensitive semiconductor wafer, further comprising:a projection optical system arranged downstream of the reflective reticle and configured to receive reflected EUV radiation from the reflective reticle and form therefrom the patterned image on the photosensitive semiconductor wafer. 21. A method of cooling a grazing-incidence collector (GIC) shell having a back surface and a central axis, comprising:providing a cooling fluid to a plurality of cooling fluid input locations adjacent the shell back surface; andguiding the cooling fluid over a portion of the shell back surface via plurality of separate pairs of substantially semicircular paths in substantially parallel planes that are substantially perpendicular to the central axis and in thermal contact with the shell back surface to a corresponding plurality of cooling fluid output locations adjacent the shell back surface and located substantially 180° from the cooling fluid input locations. 22. The method of claim 21, further comprising:defining the plurality of separate pairs of semicircular cooling fluid flow paths with a corresponding plurality of cooling lines in thermal contact with the shell back surface; andelectroforming the plurality of cooling lines onto the shell back surface. 23. The method of claim 22, wherein at least some of the cooling lines have different diameters. 24. The method of claim 22, including providing at least some of the cooling lines with non-circular cross-sections. 25. The method of claim 22, further comprising controlling the flow of cooling fluid in at least one of the cooling lines using at least one flow-control device. 26. The method of claim 21, further comprising:providing the cooling fluid to the input locations via an input cooling-fluid manifold; andcollecting the cooling fluid at the output points at an output cooling-fluid manifold. 27. The method of claim 26, further comprising fluidly connecting the cooling lines to the input and output cooling manifolds using a hydrogen retort and brazing process. 28. The method of claim 21, wherein the GIC shell has an edge and further comprising providing at least one pair of semicircular cooling fluid flow paths immediately adjacent the shell edge. 29. A method of forming a cooled, grazing incident collector (GIC) shell having a backside and a central axis, comprising:providing the shell on a mandrel;providing a cooling assembly having a plurality of substantially circularly configured cooling lines arranged in substantially parallel planes that are substantially perpendicular to the shell central axis, with each cooling line having a pair of substantially semicircular sections defined by cooling fluid input and output locations;disposing the cooling assembly such that the cooling lines contact the shell back surface;electroforming the cooling lines to the shell back surface; andremoving the shell and the attached cooling assembly from the mandrel. 30. The method of claim 29, wherein providing the shell comprises forming the shell by electroforming the shell onto the mandrel, with the mandrel having a separation layer provided thereon to facilitate said removing act. 31. The method of claim 29, wherein providing the cooling assembly includes subjecting the cooling assembly to a firing process that burns off contaminants. 32. The method of claim 29, wherein providing the cooling assembly includes forming alloy joints at the input and output locations using a hydrogen retort and a brazing process. 33. The method of claim 29, further including rotating the cooling assembly and the GIC shell during electroforming. 34. The method of claim 29, further including fluidly connecting the cooling lines to input and output cooling-fluid manifolds using a hydrogen retort and brazing process. 35. A method of collecting extreme ultraviolet (EUV) radiation from an EUV radiation source, comprising:arranging relative to the EUV radiation source a grazing-incidence collector (GIC) mirror system having at least one GIC shell;cooling the at least one GIC shell with the cooling method of claim 29; andusing the GIC mirror system to reflect the EUV radiation from the EUV radiation source to an intermediate focus.