# Patent

## Title
Multi mirror system for an illumination system

## Abstract

There is provided a multi-mirror-system for an illumination system, especially for lithography with wavelengths ≦193 nm. The system includes light rays traveling along a light oath from an object plane to an image plane, and an arc-shaped field in the image plane, whereby a radial direction in the middle of the arc-shaped field defines a scanning direction. The first mirror and the second mirror are arranged in the light path in such a position and having such a shape, that the edge sharpness of the arc-shaped field in the image plane is smaller than 5 mm in the scanning direction. Furthermore, the light rays are impinging on the first mirror and the second mirror with incidence angles ≦30° or ≧60° relative to a surface normal of the first and second mirror.

## Background
CROSS-REFERENCE TO RELATED APPLICATIONS
The present application is a continuation of U.S. application Ser. No. 10/060,909, filed on Jan. 30, 2002, now U.S. Pat. No. 6,840,640, which is a continuation of PCT/EP00/07258, filed on Jul. 28, 2000. PCT/EP00/07258 claimed priority of German Patent Application No. 199 35 568.1, filed on Jul. 30, 1999, and German Patent Application No. 299 15 847.0, filed on Sep. 9, 1999. The content of all of the above applications is hereby incorporated by reference.


BACKGROUND OF THE INVENTION
1. Field of the Invention
The invention relates to a multi-mirror-system for an illumination system, especially for lithography with wavelengths ≦193 nm comprising an imaging system.
2. Description of the Related Art
EUV-lithography constitutes one of the most promising candidates for next generation lithography. The evolution of semiconductor fabrication demands reduced feature sizes of 50 nm and beyond. This resolution is obtained by the application of a short wavelength of 13.5 nm and moderate numerical apertures of 0.2 to 0.3. The image quality of the lithography system is determined by the projection optics as well as by the performance of the illumination system. Illumination system design is one of the key challenges of EUV lithography. In today's lithographic systems, the illuminator has to deliver invariant illumination across the reticle field. For EUV, several additional requirements have to be addressed.
EUV imaging systems need to be realized as reflective optical systems. For this reason, an unobscured pupil and a highly corrected image field can only be achieved in a small radial range of the image. Hence the field shape is a ring-field with high aspect ratio of typically 2 mm (width)×22-26 mm (arc length) at wafer level. The projection systems operates in scanning mode.
EUV illumination systems will in general be non-centred systems formed by off-axis segments of aspherical mirrors. The reflectivity of multilayer-coated surfaces is approximately 70% for normal incidence and 90% for grazing incidence. In order to maximize throughput, the number of reflections has to be minimized and grazing incidence elements should be used whenever possible.
In order to achieve the requirements of the illumination system with a limited number of optical components, the complexity of the components has to be increased. Consequently, the surfaces will be segmented or aspherical. The shape and size of aspherical mirrors and segmented elements, together with stringent requirements for the surface quality put a major challenge on manufacturing these components.
Several EUV-light sources are currently being discussed. They differ in system aspects, but also in important illuminator-related aspects. System aspects are e.g. output power, repetition rate, footprint. For the illumination system size and divergence of the radiating plasma, radiation characteristics and geometrical vignetting are relevant. The illumination design has to account for these properties.
It is well known from basic physics that the étendue is invariant in optical systems. The étendue delivered by the source has to be smaller than the étendue of the illuminator, otherwise light will be lost. For current sources, however, the étendue is approximately one order of magnitude smaller, therefore either field or pupil of the optical system is not filled completely. In addition, the ring-field with high aspect ratio requires an anamorphotic étendue, which has to be formed by the illuminator.
According to Helmholtz-Lagrange, the product of field A and numerical aperture NA is invariant in classical optical systems. For unobscured and circular pupils the Helmholtz-Lagrange-Invariant HLI or étendue can be written as:

étendue=A·π·NA2  (1)

In general, the invariance of the étendue can be interpreted as the optical equivalent to the invariance of the phase space volume in conservative systems. The étendue can be written as a volume integral in four dimensions,

étendue=∫F(x,y,Px,Py)dxdydPxdPy  (2)

with the function F describing the occupied volume in phase space and

 P=(n sin θ cos φ,n sin θ sin φ,n cos θ)

the vector of optical direction cosines, which corresponds to the pupil coordinates.

For centred systems, the optical direction cosine integration in equation (2) can be written in polar coordinates (θ, φ):




  
    
      
        
          
            
              
                
                  e
                  '
                
                ⁢
                tendue
              
              =
              
                ∫
                
                  
                    F
                    ⁡
                    
                      (
                      
                        x
                        ,
                        y
                        ,
                        θ
                        ,
                        φ
                      
                      )
                    
                  
                  ⁢
                  
                    d
                    A
                  
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                    
                    
                      
                        ∂
                        
                          (
                          
                            
                              P
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                        ∂
                        
                          (
                          
                            θ
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                    d
                    θ
                  
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                    d
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              =
              
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                        y
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                      )
                    
                  
                  ⁢
                  
                    d
                    A
                  
                  ⁢
                  
                    
                  
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                  sin
                  ⁢
                  
                    
                  
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                  θ
                  ⁢
                  
                    
                  
                  ⁢
                  cos
                  ⁢
                  
                    
                  
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                  θ
                  ⁢
                  
                    d
                    θ
                  
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                    d
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        (
        3
        )
      
    
  




The illumination field at the reticle is arc-shaped with dimensions of approx. 8 mm×88 mm. Thus the étendue to be provided by the illumination system has to be almost isotropic in angular domain, but highly anamorphotic in space domain with an aspect ration of 1:10. The different light sources, however, show an almost isotropic behaviour in space as well as in angular domain. In addition, the étendue of all known light sources is too small, although an optimum collection efficiency is assumed. In EUV illumination systems it is therefore essential to transform the étendue of the light source without changing the isotropy in angular domain. Array elements offer the most promising methods to transform the étendue. With optical array elements the field formation with high aspect ratio as well as the filling of the required aperture can be achieved.
The étendue is not increased, but only transformed by the introduction of a segmentation in the entrance pupil. Examples for array elements are the ripple-plate (an array of cylindrical lenses) and the fly's eye-integrator. Both are capable of forming a field with high aspect ratio and introduce a segmentation in the entrance pupil. Partial coherent image simulations show that, the influence of the segmentation of the pupil can be tolerated, as far as a reasonable number of segments is chosen. Illumination systems with fly's-eye integrator are described in DE 199 03 807 A1 and WO 99/57732, the content of said applications is incorporated herein by reference.
Illumination systems with ripple plates are known from Henry N. Chapman, Keith A. Nugent, “A novel Condensor for EUV Lithography Ring-Field Projection Optics”, Proceedings of SPIE 3767, pp. 225-236, 1999.
The content of said article is also fully incorporated herein by reference.
The illumination system has to be combined with the lens system and it has to meet the constraints of the machine layout The mechanical layout of non-centred reflective systems strongly depends on the number of mirrors and the folding angles. Within this setup, the mirrors and special components must be mounted with tight tolerances. Heat load and natural frequencies of the frame structure have to be considered.
In EUV, each reflection will suffer from 30% light loss. The light is absorbed or dissipated leading to a heating of the mirrors. To avoid deformations of the optical elements as well as the mechanical structure, a cooling of mirrors is required. This is especially challenging because the complete optical system has to be under vacuum and hence only conduction can be used for cooling.
Furthermore in an illumination system for lithography it is desirable to introduce means for cutting off the field e.g. by a field stop.
An illumination system for lithography with a field stop is shown in U.S. Pat. No. 4,294,538. The content of said document is incorporated herein fully by reference. The system according to U.S. Pat. No. 4,294,538 comprises a slit plate on which an arcuate image of the light source is formed. By varying the radial length and the length in direction of the circular arc of the opening of the slit it is possible to adjust the radial length and the length in the direction of the circular arc of the arcuate image of the light source on a mask. Therefore the slit plate can also be designated as a field stop. Between the slit plate and the mask there are two mirrors arranged for imaging the arc-shaped field in the plane of the slit plate onto a reticle-mask.
Since the illumination system known from U.S. Pat. No. 4,294,538 is designed for a light source comprising a ultra high tension mercury lamp emitting light in the visible region the system is totally different to a illumination system for wavelengths ≦193 nm.
For example said system has no means for enhancing the étendue of the light source e.g. by raster elements of a fly's-eye integrator, which is essential for EUV-systems.
The mirrors according to U.S. Pat. No. 4,294,538 are impinged by the rays travelling through the system under an angle of 45°, which is not possible in EUV-systems, since normal incidence mirrors in EUV-systems are comprising more than 40 pairs of alternating layers. A large number of alternating layers leads to phase effects if the mean angle of incidence becomes more than 30° or is lower than 70°. Using an angle of incidence of 45° in an EUV-system as in the state of the art would lead to a total separation of s- and p-polarisation and one of both polarisation is lost completely according to Brewster law. Furthermore such a mirror would function as a polarizing element.
Another disadvantage of the system according to U.S. Pat. No. 4,294,538 are the rays impinging the reticle in the object plane telecentric, which is not possible in EUV-systems using a reflection mask.
Furthermore the system known from U.S. Pat. No. 4,294,538 is a 1:1 system. This means that the field stop in the object plane of the imaging System has the same size as the field in the image plane. Therefore the field stop has always to be moved with the same velocity as the reticle in the image plane. Furthermore said illumination system should be applicable in high throughput systems working with much higher velocities of reticle and mask than conventional systems e.g. systems known from U.S. Pat. No. 4,294,538.
SUMMARY OF THE INVENTION
Object of the invention is to provide an imaging system imaging an object, e.g. a field stop into an image, e.g. a reticle-mask for an illumination system for lithography with wavelengths ≦193 nm. Especially losses should be minimized, while the quality of the image especially regarding edge sharpness in scanning direction should be as high as possible.
Said object of the invention is solved in a first embodiment by a multi-mirror-system comprising an imaging system with at least a first and a second mirror, whereby said first mirror and said second mirror are arranged in the optical path of the imaging system in such a position and having such a shape, that the edge sharpness of the arc-shaped field in the image plane is smaller than 5 mm, preferably 2 mm, most preferably 1 mm in scanning direction.
In an advantageous embodiment the edge sharpness of the arc-shaped field in the image plane is smaller than 5 mm, preferably 2 mm, most preferably 1 mm also in the direction perpendicular to the scanning direction.
While the field in the image plane is always arc-shaped, in an first embodiment of the invention the object in the object plane is also an arc-shaped field; which means that the inventive imaging system is not comprising any field forming components.
Advantageously the rays travelling from the object plane to the image plane in the imaging system are impinging the first and the second mirror defining a first and a second used area on the mirrors, whereby the rays are impinging the first and the second mirror in the used area with an incidence angle relative to the surface normal of the mirror ≦30° or ≧60°, especially ≦20° or ≧70°, in order to minimize light losses in the system. To move the field stop in the object plane and the reticle in the image plane of the imaging system with different velocities the magnification ratio of the imaging system is unequal to 1.
In a preferred embodiment the inventive imaging system is a non centred system.
Advantageously an aperture stop is located on or close to the plane conjugate to the exit pupil of the imaging system.
Preferably the first and/or the second mirror of the imaging system is an aspheric mirror.
In a preferred embodiment of the invention the first mirror is a concave mirror having a nearly hyperbolic form or a nearly elliptic form and is defining a first axis of rotation.
Furthermore also the second mirror is a concave mirror having a nearly hyperbolic form or a nearly elliptic form and is defining a second axis of rotation.
Preferably the first and the second mirror are comprising a used area in which the rays travelling through the imaging system are impinging the first and the second mirror; the used area is arranged off-axis in respect to the first and second axis of rotation.
In advantageous embodiment the first axis of rotation and the second axis of rotation subtend an angle γ. Said angle γ is calculated from a COMA-correction of the system. The first mirror and the second mirror are defining a first magnification for the chief ray travelling through the centre of the field and the centre of the exit pupil, a second magnification for the upper COMA ray travelling through the centre of the field and the upper edge of the exit pupil and a third magnification for the lower COMA ray travelling through the centre of the field and the lower edge of the exit pupil. If the system is COMA corrected the first, the second and the third magnification are nearly identical. Said condition defines the angle γ between the first and the second axis of rotation.
In an second embodiment of the invention a multi-mirror-system for an illumination system with wavelengths ≦193 nm is comprising an imaging system, whereby said imaging system comprises at least a first mirror and a field forming optical component In such an embodiment of the invention the field in the object plane can be of arbitrary shape, e.g. a rectangular field.
In case of a rectangular field the rectangular field is formed into an arc-shaped field in the image plane by the field forming optical component of the imaging system. The advantage of the second embodiment of the invention is the fact, that no extra optical components for forming the field in the light path arranged before the inventive multi-mirror-system are necessary. This reduces the total number of mirrors in the illumination system and therefore the losses within the illumination system.
Preferably the aforementioned field forming component of the second embodiment comprises at least one grazing incidence mirror. Grazing incidence mirrors have the advantage that they must not be coated, whereas normal incidence mirrors in the EUV-range are always multilayer systems with high losses.
In a preferred embodiment the field forming component comprises two mirrors, a first grazing incidence mirror with positive optical power and a second grazing incidence mirror for rotating the field.
Another preferred embodiment employs a single grazing incidence field lens with negative optical power to achieve an arc-shaped field with the desired orientation.
Apart from the imaging system the invention provides an illumination system, especially for lithography with wavelengths ≦193 nm with a light source, a multi-mirror system comprising an imaging system, whereby the imaging system comprises an object plane. The illumination system further comprises an optical component for forming an arc-shaped field in the object plane of the multi-mirror-system, in the light path arranged before the multi-mirror system. The multi-mirror-system is a system according to the invention for imaging the field from the object plane into the image plane of the imaging system.
To enhance the étendue said illumination system could comprise at least one mirror or one lens which is or which are comprising raster elements for forming secondary light sources.
The aforementioned illumination system could be used in an EUV projection exposure unit comprising a mask on a carrier system, said mask being positioned in the image plane of the imaging system, a projection objective with an entrance pupil, said entrance pupil is situated in the same plane as the exit pupil of the illumination system and a light sensitive object on a carrier system.



DESCRIPTION OF THE DRAWINGS
Preferred embodiments of the invention are described with regard to the following figures.
In the figures are shown:
FIGS. 1 and 2: complete illumination system with an imaging system according to the invention and an arc-shaped field in the object plane of the imaging system
FIG. 3: a schematic view of the inventive illumination system
FIGS. 4 to 7: schematic views of the inventive illumination system with abbreviation used for the derivation of the COMA correction of the system
FIG. 8: detailed view of a COMA-corrected system
FIG. 8.1: arc-shaped field in the image plane
FIGS. 8.2 and 8.3: spot diagrams of the system according to FIG. 8 in the image plane
FIG. 9: detailed view of a system with correction of COMA, astigmatism and spherical aberration and a magnification of −1.0
FIGS. 9.1 to 9.2: spot diagrams of the system according to FIG. 9 in the image plane
FIG. 10: detailed view of a system with correction of COMA, astigmatism and spherical aberration of −0.85
FIG. 10.1 to 10.2: spot diagrams of the system according to FIG. 10 in the image plane
FIG. 11: EUV-illumination system with an inventive imaging system and a ripple plate as field forming component
FIG. 12: detailed view of a COMA corrected imaging system with a magnification β=−1.5
FIGS. 12.1 to 12.2: spot diagram of a system according to FIG. 12 in the image plane
FIG. 13: detailed view of an imaging system with a magnification β=−1.5 and correction of COMA, astigmatism and spherical aberration
FIGS. 13.1 to 13.2: spot diagram of a system according to FIG. 13 in the image plane
FIG. 14: schematic view of an imaging system comprising a normal and a grazing incidence mirror as field forming component
FIG. 15: schematic view of an imaging system comprising two normal and a grazing incidence mirror as field forming component
FIG. 16: view of the field in the object- and the image plane with field stop or REMA-blades
FIG. 17: detailed view of a system according to FIG. 15
FIG. 17.1: spot diagram of a system according to FIG. 17
FIG. 18: detailed view of a system according to FIG. 16
FIG. 18.1: spot diagram of a system according to FIG. 18



DESCRIPTION OF THE INVENTION
In FIG. 1 an EUV-illumination system comprising an inventive imaging system 1 comprising an object plane 3, a first mirror 5, a second mirror 7 and an image plane 9 is shown. In the object plane 3 the field stop of the system is located. Furthermore the field in the object plane 3 is already arc-shaped. The imaging system 1 images the arc-shaped field from the object plane 3 into the image plane 9. In the image plane 9 the reticle or mask of the EUV-illumination system is located. Also shown is the exit pupil 10 of the imaging system 1, which is identical with the exit pupil of the total EUV-illumination system. The exit pupil 10 falls together with the entrance pupil of the projection optical system. Furthermore the EUV-illumination system shown in FIG. 1 comprises a light source 12, a collector 14, means 16 for enhancing the étendue of the light source 12 and field forming mirrors 18, 20 for forming the arc-shaped field in the object plane 3 of the imaging system 1. Also shown are a first plane 40 conjugate to the exit pupil 10 and a second plane 42 conjugate to the exit pupil 10. Furthermore the distance eP0 between first field forming mirror 18 and the first plane 40 conjugated to the exit pupil 10, the distance e01 between the first 18 and the second 20 field forming mirror, the distance SE1′ between the second field forming mirror 20 and the second plane 42 conjugate to the exit pupil 10, the distance SR1′ between the second field forming mirror 20 and the object plane 3 and the distance SE2 between the second plane 42 conjugate to the exit pupil 10 and the first imaging mirror 5 is depicted.
Throughout the system examples shown hereinafter some parameters remain constant The design principles as shown below however, can also be applied to other sets of parameters.
In all embodiments shown in this application the incidence angle at the image plane 9 of the imaging system is 6° and the numerical aperture at the image plane 9 is NA=0.05. It corresponds for example to a NA=0.0625 of the projection lens and a σ=0.8. The projection lens arranged in the light path after the EUV-illumination system has typically a 4×-magnification and thus NA=0.25 at the light sensitive object e.g. the wafer of the EUV-projection exposure unit.
FIG. 2 shows the EUV-illumination system depicted schematic in FIG. 1 in greater detail. Same components as in FIG. 1 are designated with the same reference numbers.
The system according to FIG. 2 comprises a light source 12 and a collector-mirror 14. Regarding the possible EUV-light sources reference is made to DE 199 038 07 A1 and WO 99/57732, the content of said documents is incorporated herein by reference. The collector mirror 14 of the system according to FIG. 2 is of elliptical shape. The means 16 for enhancing the étendue comprises two mirrors with raster elements 30, 32 so called fly-eyes integrators. The first mirror with raster elements 30 comprises an array of 4×64 field facets; each field facet being of plane or elliptical, toroidal or spherical shape (R≈−850 mm). The second mirror with raster elements 32 comprises an array of 16×16 pupil facets or a spherical or hexagonal grid with pupil facets, each pupil facet being of hyperbolic, toroidal or spherical shape (R≈−960 mm). The second mirror 32 is located in a plane conjugate to the exit pupil 10 of the illumination system.
An illumination system with a first and a second mirror comprising raster elements as described before is known from DE 199 038 07 A1 and WO 99/57732; the content of said applications is incorporated herein by reference.
For forming the arc shaped field in the object plane of the imaging system comprises two field forming mirrors 18, 20. The second field forming mirror 20 is a grazing incidence mirror.
In principle one mirror, here the mirror 20, would be sufficient for field forming. But mirror 18 is required to control the length of the system and the size of the pupil facets. In order to achieve a large field radius of ≈100 mm mirror 20 must have low optical power.
The size of the field and the pupil facets are related to the étendue of the system. The product of the size of the field facets and the size of the pupil plane is determined by the étendue. The pupil plane is a first plane 40 conjugate to the exit pupil 10 of the illumination system. In said plane the second mirror with raster elements 32 is located. Due to the aforementioned relation restrictions to the size of the field facets and the pupil facets are given. If the magnification for the pupil facets is very large, i.e. the pupil facet is very small, field facets become very large. To avoid large magnification of the imaging of the pupil facets into a second plane 42 conjugate to the exit pupil 10 of the system either the distance between mirror 20 and the second mirror with raster elements 32 increases or an additional mirror 18 has to be introduced. The first field forming mirror 18 has almost all power of the imaging system consisting of a first field forming mirror 18 and a second mirror 20 for imaging the pupil facets of the second field forming mirror with raster elements 32 into the second plane 42 conjugate to the exit pupil 10 of the system.
The data for the first field mirror 18 and the second field mirror 20 are given in table 1:







TABLE 1







Data for the first and the second field mirror










first field mirror 18
second field mirror 20





shape
hyperbola
ellipsoid


f
≈1616 mm
≈605 mm


incidence angle versus
7°
75°


surface normal

(grazing incidence)


conic section layout
for pupil imaging
for pupil imaging


βpupil imaging
7.46429
−0.05386









The magnification between the first plane 40 conjugate to the exit pupil 10 and the second plane 42 conjugate to exit pupil 10 is β40→42≈−0.4. The field radius of the arc-shaped field in the object plane 3 is controlled by the second field mirror 20.
If the magnification βimage=−1 of the imaging system and RField=100 mm the field radius to be formed by the second field forming mirror 20 is RObj=−100 mm. There are three means to control the radius RObj: The optical power, see table 1,
f≈605 mm, the chief ray distance between the second field forming mirror 20 and the object plane 3:
SR1′≈250 mm and the grazing incidence angle.
With the further values for the system layout
eP0=1400 mm
e01=1550 mm
SE1′≈637 mm
SF2≈−262.965 mm
the system can be derived with first order optical formulas.
In the second plane 42 conjugate to the exit pupil 10 an accessible aperture stop for the illumination system could be located.
Also shown in FIG. 2 is the inventive multi-mirror-system comprising an imaging system 1 with a first 5 and a second 7 imaging mirror for imaging the arc-shaped field from the object plane 3, which is conjugate to the field plane, into the image plane 9, which corresponds to the field plane of the illumination system and in which the reticle or mask of the illumination system is located.
The conjugate field plane 3 could be used as a plane for reticle masking. Said plane is located near to the second field forming mirror 20 at the limit for construction, e.g. SR′≈250 mm chief ray distance for ≈15° grazing incidence reflection on the mirror. The field in the conjugate field plane which is the object plane 3 is arc-shaped by field forming mirror 20, thus rema blades need to be almost rectangular. Small distortions of a following rema system can be compensated for.
Since all mirrors of the illumination system have positive optical power, the field orientation in the conjugate field plane 3 after positive mirror 20 is mirrored by negative magnification of the inventive imaging system 1. The field orientation in the field plane 9 is then correct.
Since the second field forming mirror 20 is off-axis in order to compensate the distortion due to this off-axis arrangement, the pupil facets have to be arranged on the second mirror with raster elements 32 on a distorted grid.
With pupil facets arranged on a pre-distorted grid optimized pupils with respect to telecentricity and ellipticity can be achieved.
The derivation of a multi-mirror-system comprising an imaging system for imaging a REMA-blade situated in the object-plane or REMA-plane 3 of the inventive multi-mirror-system into the image plane or field plane 9, wherein the reticle is situated will be described in detail hereinbelow.
FIG. 3 shows in a schematic refractive view the elements of the inventive imaging system and abbreviations used in table 1. Furthermore components with reference numbers used in FIGS. 1 and 2 are designated with the same reference numbers. Furthermore in FIG. 3 is shown the virtual image 3′ of the field plane and the virtual image 10′ of the exit pupil.
The imaging system according to FIG. 3 and table 2 is a hyperbolic-ellipsoid combination as a first order starting system. The data of the first order system are given in table 2.







TABLE 2







First order system layout












second




Hyperboloid
imaging
Ellipsoid


first Imaging mirror 5
field imaging
mirror 7
pupil imaging














e23
650.0



f
768.1818
f
650.0







Pupil imaging










SE2
−262.9651
SE3
−1049.8383


SE2′
−399.8383
SE3′
1706.6772


β2
1.5205
β3
−1.6257







Field imaging










SR2
−650.0
SR3
−4875.0


SR2′
−4225.0
SR3′
750.0


β2
6.5
β3
−0.15385









For the results of table 2, well-known first-order lens-formulas where used, e.g.




  
    
      
        
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            S
          
        
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            S
            
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                ,
                
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          f
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            ⁢
            
              
            
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              (
              
                
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                      -
                    
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                    maker
                  
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                equation
              
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        (
        4
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where S and S′ stands for SE and SE′ or SR and SR′, respectively.

In the next step designing an imaging system according to the invention the first order system shown in table 2 is optimized and COMA corrected.
The first mirror 5 of the imaging system is a hyperbolic mirror, optimized for field imaging, which means imaging of the field in the REMA plane 3 into the field plane 9. The second mirror 7 of the imaging systems is an elliptical mirror optimized for pupil imaging, which means imaging of the second plane 42 conjugate to the exit pupil into the exit pupil 10. The overall system comprising the first 5 and the second 7 imaging mirror with abbreviations used in table 3 for the COMA corrected system is shown in FIGS. 3 to 5. Identical components as in FIG. 1, FIG. 2 and FIG. 3 are designated with the same reference numbers.
Apart from the elements already shown in FIGS. 1 and 2 in FIG. 3; FIG. 4 shows:

    
    
        the axis of rotation 50 of the first imaging mirror 5
        the axis of rotation 52 of the second imaging mirror 7
        the centre 54 of the first imaging mirror
        the vertex of the first imaging mirror 56
        the virtual image 3′ of the field plane 3
        the centre 58 of the second imaging mirror
        the vertex of the second imaging mirror 60
        the virtual image 10′ of the exit pupil 10 of the illumination system
        the chief ray 62
    
    


As is apparent from FIG. 4 the axis 50 of the hyperbolic mirror 5 and the axis of the elliptic mirror 7 subtend an angle γ.
FIG. 5 shows in detail the first imaging mirror 5, which is in this embodiment a hyperboloid, of the inventive imaging system according to FIG. 4 and FIG. 6 the second imaging mirror 7 of the imaging system according to FIG. 4, which in this embodiment is a ellipse. The same elements as in FIG. 4 are designated in FIG. 5 and FIG. 6 with the same reference numbers.
In FIG. 5 depicting the first hyperbolic mirror 5 the abbreviation used for the following equations calculating the parameters of the hyperbola are known:
With positive angles ω2 and δ2 follows

d2=−SR2·sin(ω2)=−SR2′·sin(δ2)  (5)

ω2=2α2−δ2  (6)





  
    
      
        
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                        2
                      
                    
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                  sin
                  ⁢
                  
                    
                  
                  ⁢
                  
                    (
                    
                      2
                      ⁢
                      
                        α
                        2
                      
                    
                    )
                  
                
                
                  tan
                  ⁢
                  
                    
                  
                  ⁢
                  
                    (
                    
                      δ
                      2
                    
                    )
                  
                
              
              -
              
                cos
                ⁢
                
                  
                
                ⁢
                
                  (
                  
                    2
                    ⁢
                    
                      
                    
                    ⁢
                    
                      α
                      2
                    
                  
                  )
                
              
            
          
        
      
    
    
      
        (
        7
        )
      
    
  
  
    
      
        
          ⇒
          
            δ
            2
          
        
        =
        
          arctan
          ⁡
          
            (
            
              
                sin
                ⁢
                
                  
                
                ⁢
                
                  (
                  
                    2
                    ⁢
                    
                      
                    
                    ⁢
                    
                      α
                      2
                    
                  
                  )
                
              
              
                
                  β
                  field
                
                +
                
                  cos
                  ⁢
                  
                    
                  
                  ⁢
                  
                    (
                    
                      2
                      ⁢
                      
                        
                      
                      ⁢
                      
                        α
                        2
                      
                    
                    )
                  
                
              
            
            )
          
        
      
    
    
      
        (
        8
        )
      
    
  




Then the angle between incident chief ray and hyperbola axis is:

ω2=2α2−δ2 

Hyperbola Equation:





  
    
      
        
          
            
              
                z
                2
              
              
                a
                2
              
            
            -
            
              
                d
                2
              
              
                b
                2
              
            
          
          =
          1
        
        ;
        
          a
          =
          
            
              
                e
                2
              
              -
              
                b
                2
              
            
          
        
      
    
    
      
        (
        9
        )
      
    
  




insertion and solution for b2 gives:

b4+(z2+d2−e2)b2−d2=0  (10)





  
    
      
        
          ⇒
          
            b
            2
          
        
        =
        
          
            
              -
              
                (
                
                  
                    z
                    2
                  
                  +
                  
                    d
                    2
                  
                  -
                  
                    e
                    2
                  
                
                )
              
            
            +
            
              
                
                  
                    (
                    
                      
                        z
                        2
                      
                      +
                      
                        d
                        2
                      
                      -
                      
                        e
                        2
                      
                    
                    )
                  
                  2
                
                -
                
                  4
                  ⁢
                  
                    d
                    2
                  
                  ⁢
                  
                    e
                    2
                  
                
              
            
          
          2
        
      
    
    
      
        (
        11
        )
      
    
  




with equation (5) and

z2=e+SR2·cos(ω2)  (12a)





  
    
      
        e
        =
        
          
            (
            
              
                
                  
                    -
                    SR2
                  
                  ·
                  cos
                
                ⁢
                
                  
                
                ⁢
                
                  (
                  
                    ω
                    2
                  
                  )
                
              
              -
              
                
                  
                    SR2
                    ′
                  
                  ·
                  cos
                
                ⁢
                
                  
                
                ⁢
                
                  (
                  
                    δ
                    2
                  
                  )
                
              
            
            )
          
          2
        
      
    
    
      
        (
        
          12
          ⁢
          b
        
        )
      
    
  




the parameters defining the hyperbola can be calculated.

In FIG. 6 depicting the second elliptic mirror 7 the abbreviations used for the following equations calculating the parameters of the ellipse are shown:
With positive angles ω3 and δ3 follows

d3=−SE3·sin(ω3)=+SE3′·sin(δ3)  (13)

ω3=2α3+δ3  (14)





  
    
      
        
          ⇒
          
            -
            
              β
              pupil
            
          
        
        =
        
          
            
              SE3
              ′
            
            
              -
              SE3
            
          
          =
          
            
              
                sin
                ⁢
                
                  
                
                ⁢
                
                  (
                  
                    
                      2
                      ⁢
                      
                        
                      
                      ⁢
                      
                        α
                        3
                      
                    
                    +
                    
                      δ
                      3
                    
                  
                  )
                
              
              
                sin
                ⁢
                
                  
                
                ⁢
                
                  (
                  
                    δ
                    3
                  
                  )
                
              
            
            =
            
              
                
                  sin
                  ⁢
                  
                    
                  
                  ⁢
                  
                    (
                    
                      2
                      ⁢
                      
                        
                      
                      ⁢
                      
                        α
                        3
                      
                    
                    )
                  
                
                
                  tan
                  ⁡
                  
                    (
                    
                      δ
                      3
                    
                    )
                  
                
              
              +
              
                cos
                ⁡
                
                  (
                  
                    2
                    ⁢
                    
                      
                    
                    ⁢
                    
                      α
                      3
                    
                  
                  )
                
              
            
          
        
      
    
    
      
        (
        15
        )
      
    
  
  
    
      
        
          ⇒
          
            δ
            3
          
        
        =
        
          arctan
          ⁡
          
            (
            
              
                -
                
                  sin
                  ⁡
                  
                    (
                    
                      2
                      ⁢
                      
                        
                      
                      ⁢
                      
                        α
                        3
                      
                    
                    )
                  
                
              
              
                
                  β
                  field
                
                +
                
                  cos
                  ⁢
                  
                    
                  
                  ⁢
                  
                    (
                    
                      2
                      ⁢
                      
                        
                      
                      ⁢
                      
                        α
                        3
                      
                    
                    )
                  
                
              
            
            )
          
        
      
    
    
      
        (
        16
        )
      
    
  




The angle between incident chief ray and the hyperbola axis is defined by equation (14).
Ellipsoid Equation:




  
    
      
        
          
            
              
                z
                2
              
              
                a
                2
              
            
            +
            
              
                d
                2
              
              
                b
                2
              
            
          
          =
          1
        
        ;
        
          a
          =
          
            
              
                e
                2
              
              +
              
                b
                2
              
            
          
        
      
    
    
      
        (
        17
        )
      
    
  




insertion and solution for b2 gives:

b4+(e2−z2−d2)b2−d2e2=0  (18)





  
    
      
        
          ⇒
          
            b
            2
          
        
        =
        
          
            
              -
              
                (
                
                  
                    e
                    2
                  
                  -
                  
                    z
                    2
                  
                  -
                  
                    d
                    2
                  
                
                )
              
            
            +
            
              
                
                  
                    (
                    
                      
                        e
                        2
                      
                      -
                      
                        z
                        2
                      
                      -
                      
                        d
                        2
                      
                    
                    )
                  
                  2
                
                -
                
                  4
                  ⁢
                  
                    d
                    2
                  
                  ⁢
                  
                    e
                    2
                  
                
              
            
          
          2
        
      
    
    
      
        (
        19
        )
      
    
  




with equation (13) and

z3=e−SE2·cos(ω3)  (20a)





  
    
      
        e
        =
        
          
            (
            
              
                
                  SE3
                  ·
                  cos
                
                ⁢
                
                  
                
                ⁢
                
                  (
                  
                    ω
                    3
                  
                  )
                
              
              +
              
                
                  SE3
                  ′
                
                ·
                
                  cos
                  ⁡
                  
                    (
                    
                      δ
                      3
                    
                    )
                  
                
              
            
            )
          
          2
        
      
    
    
      
        (
        
          20
          ⁢
          b
        
        )
      
    
  




the parameters defining the ellipsoid can be calculated.

Furthermore for ellipse and hyperbola following equations are well known:




  
    
      
        p
        =
        
          
            
              
                b
                2
              
              a
            
            ⁢
            
              
            
            ⁢
            curvature
            ⁢
            
              
            
            ⁢
            at
            ⁢
            
              
            
            ⁢
            node
            ⁢
            
              
            
            ⁢
            R
          
          =
          
            -
            p
          
        
      
    
    
      
        (
        21
        )
      
    
  
  
    
      
        ɛ
        =
        
          
            e
            a
          
          ⁢
          
            
          
          ⁢
          eccentricity
        
      
    
    
      
        (
        22
        )
      
    
  




K=−ε2 conic constant  (23)

By COMA-correcting the first order system according to table 2 with an analytical calculation angle γ is determined. The COMA-correction uses for calculating γ the magnification of the imaging for the chief ray 62 and the coma-rays not shown in FIG. 46. The differences in magnifications can be reduced by minimization of the angle of incidence α3 (7°) and corresponding selection of α2. In this example the equations are minimized by the gradient method, which means choose a start system e.g. according to table 2, calculate the magnifications, change the angle α2 and calculate a new magnifications. From the difference in magnifications the next α2 can be calculated. Repeat this algorithm until difference in magnification for the chief ray and the upper and lower COMA-ray is less than e.g. 0.5%.
The COMA-correction will be described hereinbelow in detail with reference to FIG. 7. Identical elements as in FIG. 1 to 6 are designated with the same reference numbers. Furthermore in FIG. 7 is shown the lower COMA ray 70.
The calculation of the magnifications along the chief ray 62 is clear from the first order derivation.
The calculation for the COMA or rim rays is shown with regard to the lower COMA ray 70.
The COMA rays 70 for the imaging 3→3′ at the hyperbola is straight forward. The COMA or rim rays in the object plane 3 can be defined by the angles between rays and hyperbola axis:




  
    
      
        
          ω
          
            2
            ⁢
            c
          
        
        =
        
          
            ω
            2
          
          ∓
          
            arscin
            ⁢
            
              
            
            ⁢
            
              (
              
                
                
                  
                    NA
                    reticle
                  
                  ·
                  
                    β
                    
                      rema
                      ,
                      field
                    
                  
                
                
              
              )
            
          
        
      
    
    
      
        (
        24
        )
      
    
  




with ω2 as shown in FIG. 5.

The distances between the image points 3 and 3′ and the intersection point I2c of the mirror with the COMA or rim rays are given by hyperbola formulas in polar co-coordinates:




  
    
      
        
          S
          c
        
        =
        
          
            
              RI
              
                2
                ⁢
                c
              
            
            _
          
          =
          
            p
            
              1
              +
              
                ɛ
                ⁢
                
                  
                
                ⁢
                
                  cos
                  ⁡
                  
                    (
                    
                      ω
                      
                        2
                        ⁢
                        c
                      
                    
                    )
                  
                
              
            
          
        
      
    
    
      
        (
        25
        )
      
    
  




S′c= I2cR′=Sc+2a  (26)

α, ε, p: hyperbola parameters
To calculate the lengths at the ellipse is more complicated, because the COMA or rim rays will not intersect in the plane 9 any more. However the magnification can be calculated approximately after calculating the intersection point I3c. With

ω3c=δ2c±γ  (27)

for given γ, ω3c and thus the intersection point I3c can be calculated. With

Lc= R′I3c  (28)

L′c= I3cR′′  (29)

the magnification of the rema-imaging system for the rim or COMA rays follows





  
    
      
        
          β
          
            c
            ±
          
        
        =
        
          
            
              L
              c
              ′
            
            
              L
              c
            
          
          ·
          
            
              S
              c
              ′
            
            
              S
              c
            
          
        
      
    
    
      
        (
        30
        )
      
    
  




As shown in FIG. 7 this derivation is not exact, because the rim rays will not intersect in the image plane 9 exactly. However, magnification can be calculated with reasonable accuracy, sufficient for a minimisation of the COMA error.
An optimisation with the gradient method described before leads to the solution given in table 3.







TABLE 3







COMA corrected system starting from


the system according to table 1.










first imaging mirror 5

second imaging mirror 7








Design parameters (abbreviation see FIGS. 4 to 6)













α2
16.328°
α3
7.0°


δ2
4.2034
δ3
20.26125


ω2
28.4526
ω3
34.26125


d2 = YDE
309.6806
d3 = YDE
591.0246


z2
1821.0739
z3
1234.3716


a
1787.5
a
1378.2578


b
1590.3439
b
1328.5797


e
2392.5614
e
366.7021


R
−1414.9336
R
−1280.6922


eps = e/a
1.3385
eps = e/a
0.2661


K = −eps{circumflex over ( )}2
−1.7916
K = −eps{circumflex over ( )}2
−0.0708


ZDE = z2 − a
33.5616
ZDE = a − z3
143.8861









YDE and ZDE are the y- and z-components of the decenter vector of the nearest vertex point of the conic section.
For a COMA-corrected system according to table 3 the magnification difference due to COMA is approx. 0.1% and is identical for the upper and the lower COMA-ray. The data for the magnification β of the inventive two mirror imaging system for the chief ray, the upper and lower COMA-ray after COMA correction is shown in table 4.







TABLE 4







Magnification β for chief ray, upper and lower COMA-ray


Coma-correction of Field imaging












Upper COMA-ray

Chief ray
Lower COMA-ray
















Magnification
1.0012
1.0000
1.0012










In FIG. 8 the COMA-corrected imaging system is shown. Identical elements as in FIGS. 1 to 7 are designated with the same reference numbers.
In FIG. 8.1 the arc-shaped field in the field or reticle plane with carthesian coordinates x and y is shown. Reference number 100 designates a field point in the centre of the arc-shaped field and 102, a field point at the edge of the arc-shaped field. The y-axis denotes the scanning direction and the x-axis the direction perpendicular to the scanning direction.
In FIG. 8.2 the spot diagram for a field point 100 and in FIG. 8.3 the spot diagram for a field point 102 of a COMA-corrected multi-mirror-system according to FIGS. 4 to 8 is depicted. The spot diagram is the diagram resulting from a multiplicity of rays travelling through the system with the aperture NAobject and impinging the field or reticle plane in a predetermined field point, e.g. the centre of the field 100. The aperture is NAobject=0.05 in the system described in FIGS. 4 to 8.
As is apparent from the spot-diagrams 8.2 and 8.3 the edge sharpness EDS in scanning direction, corresponding to the y-axis of the arc shaped field, in COMA corrected system is smaller than 2 mm.
The edge sharpness EDS of a system in scanning direction is defined as the difference of the points with the greatest value and the smallest value in y-direction for an edge field point, e.g. edge field point 102 as shown in FIG. 8.3.
For further optimizing the inventive imaging system astigmatism and spherical aberration has to be considered. Nevertheless a balanced system can be found with only hyperbolic and elliptical mirrors. FIG. 9 and table 5 shows a system which is corrected for spot aberrations <1 mm in scanning direction. Because the rema blades are essentially required to avoid the overscan in scanning direction, it is sufficient to achieve the required performance in scanning direction; here in y-direction.
In FIG. 9 the same elements as in FIGS. 1 to 8 are designated with the same reference numbers. In FIG. 9.1 and 9.2 the spot-diagrams for a point in the centre of the field 100 and for an edge point 102 is depicted.
The optical data of the system according to FIG. 9 are shown in table 5.
The embodiment according to FIG. 9 is again a 1:1 imaging system and is derived from the embodiment according to FIG. 8.







TABLE 5







System corrected for COMA, astigmation and spherical aberration












second





imaging


first imaging mirror 5
Hyberbola
mirror 7
Ellipse













α2
8.9395
α3
6.4304


δ2
1.9988
δ3
20.5977


ω2
15.8802
ω3
33.4585


d2 = YDE
283.1433
d3 = YDE
587.5428


a2
5949.4780
a3
1371.5001


b
2942.2505
b
1329.5276


e
6637.2529
e
336.7028


R
−1455.0585
R
−1288.8396


eps = e/a
1.1156
eps = e/a
0.2455


K = −eps{circumflex over ( )}2
−1.2446
K = −eps{circumflex over ( )}2
−0.0603


ZDE
29.4941
ZDE
143.7641









The image plane 9 comprising the reticle is tilted with respect to the chief ray by 6°-angle of incidence. For a minimized spot aberration also the object plane 3 has to be tilted. In the example the optimized tilt angle of the object plane 3, where the field stop or rema has to be placed, is approximately 0.9768°.
Also shown in FIGS. 8 and 9 are the complete first hyperbolic imaging 5 and the complete second elliptic imaging mirror 7 of the imaging system with the first axis of rotation 50 and the second axis of rotation 52. As is apparent from FIG. 9 the rays impinging the mirrors of the imaging system off-axis; this means that the used area of the two mirrors are situated off-axis with regard to the axis of rotation of the two mirrors. Also clearly shown the angle γ between the two axis of rotation.
In FIG. 10 an even better performing imaging system than the system according to FIG. 8 is shown. The same reference numbers as for the system according to FIG. 9 are used. The system according to FIG. 10 is derived from a more balanced optimization. This time the magnification is β≈−0.85.
The limiting aberrations in the imaging system according to the invention is COMA and astigmatism.
For field imaging a mirror 5 near to conjugate pupil plane 42 is used. This mirror 5 is aimed not to affect pupil imaging. If one looks at the aberrations in a plane which contains the focus, for field points different from the focus there are field aberrations. That is the case of the hyperbola, which is actually limited by astigmatism. For a given field of view size the smaller the tilt angle of the hyperbola, the smaller the angle of the field objects and, therefore, the smaller the astigmatism.
An elliptical mirror 7 is chosen for pupil imaging. The ellipse case is more complicated because the parameters are found to give stigmatic imaging at the centre of the exit pupil, not in the field plane 7. When used off axis for other conjugates different than the two geometrical foci, the ellipse introduces coma, and this is what can be seen in the field plane 7. Once more, the way of reducing this coma is minimising the tilt and balancing COMA between the first mirror 5 and the second mirror 7 of the imaging system.
The spot diagrams for the centre field point 100 and an edge field point 102 for a system according to FIG. 10 are depicted in FIGS. 10.1 and 10.2. As is apparent from FIG. 10.2 the edge sharpness EDS for an edge field point is better than 1 mm in the scanning direction as well as in the direction perpendicular to the scanning direction. Said embodiment is a preferred embodiment since the required imaging performance of the imaging system is also achieved in the direction perpendicular to the scanning direction; here in the x-direction.
The data of the system according to FIG. 10 are given in Code-V-format in table 6.







TABLE 6







Code V-table of a imaging system with β = −0.85
















Surface





!
Radius
distance to next surface
typ
















S0
  0
0
DAR;
ADE
 6.0;



S
  0
−369.481
REFL


S
  0
−110.093












S
6964.67
0
REFL
!
first imaging mirror 5



CON



K
−205.127














DAR;


ADE
−19.23631;






YDE
149.7571;
ZDE
50.40653


S
  0
0






ADE
−36.0;


S
  0
500.9524


S
  0
0






ADE
 10.0;












S
−898.3867
0
REFL
!
Second imaging mirror 7



CON



K
−0.2302684














DAR;


ADE
 5.464502;






YDE
164.4807;
ZDE
−0.638



CIR
1000


S
  0
−797


S
  0
0
REFL



BEN;


ADE
 −6.0;



CIR
500


SI
  0
0

!Reticle



DAR


ADE
 6.0









In FIG. 11 a EUV-illumination system with a ripple-plate 200 as field-forming component and an multi-mirror-system comprising an imaging system 1 according to the invention is shown. The system comprising a light source 12, a collector unit 14, a ripple-plate 200 as a field-forming component for the arc-shaped field and a field mirror (202) is known from Henry N. Chapman et al. aa.O; the content of said article is incorporated herein by reference.
The imaging system shown in FIG. 11 is identical to the imaging systems according to FIGS. 1 to 10. The same elements as in FIGS. 1 to 10 are designated with the same reference numbers.
Other setups then those of FIG. 11 are possible, in which the light is not collimated before the ripple plate 200, but converging to a focal point. In this case the grooves of the ripple plate are not parallel, but conically, i.e. the prolongation of the grooves meet in one point corresponding to the focal point of the incident wave.
The shape of the ripple plate 200 can be derived theoretically, but has to be optimized. The pupil formation with the ripple design leads to an elliptical illumination of the exit pupil after the illumination system corresponding to the entrance pupil of the lens system. Therefore an aperture stop is required in a conjugate pupil plane. This aperture stop will also lead to light less. The ellipticity of the pupil increases with the lateral coordinate, along the arc field perpendicular to scanning direction. The light loss has to be compensated for by shaping the ripple plate aspherically.
Next, two examples of hyperbola-ellipsoid-combinations for the imaging mirrors 5, 7 are shown with β=−1.5. The first order system is analytically derived, as described before. The second system is optimized for a better performance in scanning direction. The parameters are given in tables 7 to 9:







TABLE 7







First-order parameters for βrema = −1.5 - system.














second




first imaging

imaging



mirror 5
Hyberboloid
mirror 7
Ellipsoid

















e 23
650.00




f2
495.9484
f3
721.5351







pupil imaging












SE2
−271.5174
SE3
−1250.0000



SE2′
−600.0000
SE3′
1706.6772



β2
2.2098
β3
−1.3653







field imaging












SR2
−482.9048
SR3
−19011.2108



SR2′
−18361.2108
SR3′
750.0000



β2
38.0224
β3
−0.0395










If one corrects the coma of the system of table 7 according to analytic solution of ellipsoid and hyperboloid, as shown before, a system as shown in table 8 and FIG. 12 results. The spot aberrations are shown in FIG. 12.1 and FIG. 12.2 for a centre field point 100 and an edge field point 102.







TABLE 8







COMA corrected system












first imaging mirror 5

second imaging mirror 7
















α2
8.4600
α3
6.5000



δ2
0.4278
δ3
29.9146



ω2
16.4922
ω3
42.9146



d2 = YDE
137.04894
d3 = YDE
851.1340



α2
8939.1530
α3
1478.3386



b
2945.3024
b
1441.2091



e
9411.8682
e
281.9172



R
−970.4282
R
−1424.5774



eps = e/a
1.0529
eps = e/a
0.1907



K = −eps{circumflex over ( )}2
−1.1086
K = −eps{circumflex over ( )}2
−0.0364



ZDE = z − a
9.9779
ZDE = a − z
280.9593










The embodiment according to FIG. 13 and table 9 is optimized to achieve spot aberration less than 1 mm in scanning direction:







TABLE 9







Optimized design












first imaging mirror 5

second imaging mirror 7
















α2
8.0302
α3
6.2127



δ2
0.1706
δ3
30.3800



ω2
16.2310
ω3
42.8054



d = YDE
139.9744
d = YDE
848.9438



R
−967.1380
R
−1415.0130



K = −eps{circumflex over ( )}2
−1.1933
K = −eps{circumflex over ( )}2
−0.04913



ZDE = z − a
11.3839
ZDE = a − z
284.2995










In the following section an illumination system with an arbitrary field, e.g. a rectangular field in the object plane 3 is discussed. The schematic set-up for such systems are shown in FIGS. 14 and 15. In both examples the imaging system images a rectangular field 300 into an arc-shaped field 302. Consequently arc-shaped rema blades or field stop 304 have to be applied to compensate for the deformation induced by the imaging with grazing incidence field mirror 306 as shown in FIG. 16. Furthermore in FIG. 16 the clipping 308 in the image or rema-plane 9 is shown.
The system according to FIGS. 14 and 15 comprises: an object plane 3 at least, a first imaging normal incidence mirror 5 and at least one grazing incidence mirror 306 for forming the arc-shaped field in the image plane 9.
A realisation of a system with one grazing incidence mirror 306 is given in FIG. 17. To achieve the desired orientation for the ring field, a field lens with negative optical power is required. The radius of the arc-shaped field is approximately 138 mm, however, by the angle of incidence and the optical power of the first imaging mirror 5 almost any desired field radius is achievable. Table 10 gives the data for such a system, where for the magnification βimage=−1.2 was chosen.












TABLE 10









grazing






imaging



first imaging

mirror



mirror 5
ellipsoid
306
hyperboloid





















α1
12.0
α2
78.0




e 12
500.00



f1
382.1450
f2
−868.3020







pupil imaging












SE1
−609.7360
SE2
523.8000



SE1′
1023.8000
SE2′
1320.2146



β1
−1.6791
β2
2.5205







field imaging












SR1
−810.6258
SR2
222.9651



SR1′
722.9651
SR2′
300.0000



β1
−0.8919
β2
1.3455







surface parameters












δ1
27.9820
δ2
14.2042



ω1
51.9820
ω2
38.2042



e
264.2854
e
434.1220



d
480.3602
d
323.9526



b
772.8280
b
172.8956



a
816.7680
a
398.2073



p = R
−731.2519
p = R
75.0687



eps
0.3236
eps
1.0902



K
−0.1047
K
−1.1885



z
639.8277
z
845.7300










The arcuate field is demonstrated in FIG. 17.1. A rectangular aperture was ray-traced through the system until the reticle plane. Here the arc-shaped field arises due to the grazing incidence reflection at the grazing incidence mirror 306. However, the spot diameter is in this un-optimized example about 10 mm. Due to the imaging with one normal incidence and one grazing incidence mirror, a large amount of coma is introduced, which can not be reduced effectively.
A reduction of coma is possible by insertion of a second normal incidence mirror 7. An example is shown in FIG. 18, the corresponding data are given in table 11 (with βimage=−1.272). The illumination at reticle field is shown in FIG. 18.1. The system has capability to be optimized further to similar performance as system examples given before by similar straight forward optimization, which means proper selection of reflection and folding angles.












TABLE 11







second

grazing



first imaging

imaging

incidence


mirror 5
ellipsoid
mirror 7
hyperboloid
mirror
hyperboloid




















α0
8.0
α1
11.0
α2
12.0



e01
450.0000
e12
500.000


f0
686.2745
f1
1055.0641
f2
−868.302







pupil imaging












SE0
−700.0360
SE1
3455.9
SE2
523.8


SE0′
35000.0
SE1′
1023.8
SE2′
1320.2146


β0
−50.0
β1
0.0296
β2
2.5205







field imaging












SR0
−914.8405
SR1
2296.8290
SR2
222.9651


SR0′
2746.8290
SR1′
722.9651
SR2′
300.0


β0
−3.0025
β1
0.3148
β2
1.3455


δ0
7.6903
δ1
21.3810193242
δ2
14.2042


ω0
23.6903
ω1
0.6189806758
ω2
38.2042


b
1569.789
b
5838.1891964484
b
172.8956


a
1830.8348
a
16763.1000000000
a
398.2073


p = R
−1345.9639
p = R
−2033.3024973619
p = R
−75.0687


eps
0.5146
eps
1.0589128053
eps
1.0902


K
−0.2448
K
−1.1212963293
K
−1.1885


e
942.1881
e
17750.6612469375
e
434.122


d
367.5763
d
373.24505478583
d
323.9526


z
1779.9356
z
−16797.3226034857
z
845.73









REFERENCE NUMBERS


    1: imaging system
    3: object plane=field plane
    3′: virtual image of the field plane
    5: first imaging mirror
    9: image plane
    10: exit pupil
    10′: virtual image of the exit pupil
    12: light source
    14: collector
    16: means for enhancing the entendu
    18: first field forming mirrors
    20: second field forming mirrors
    30: first mirror with raster elements
    32: second mirror with raster elements
    40: first plane conjugate to the exit pupil
    42: second plane conjugate to the exit pupil
    50: axis of rotation of the first imaging mirror
    52: axis of rotation of the second imaging mirror
    54: centre of the first imaging mirror
    56: vertex of the first imaging mirror
    58: centre of the second imaging mirror
    60: vertex of the second imaging mirror
    62: chief ray
    70: lower COMA ray
    100: field point in the centre of the arc shaped field
    102: field point at the edge of the arc shaped field
    200: ripple plate
    300: rectangular field
    302: arc shaped field
    304: field stop
    306: grazing incidence mirror
    308: clipping
    eP0: distance between first mirror and first plane conjugate to the exit plane
    e01: distance between first and second field forming mirror
    EDS: edge sharpness
    SE1′: distance between second field forming mirror and second plane conjugate to the exit pupil
    SR1′: distance between second field forming mirror and object plane
    SE2: distance between second plane conjugate to the exit pupil and first imaging mirror
    x: direction perpendicular to the scanning direction
    y: direction in scanning direction
    γ: angle between the axis of rotation 50, 52
    fi: focal length of optical component i
    αi: angle of incidence of chief ray with respect of surface normal of mirror i
    βpupil: magnification for pupil imaging between conjugate pupil planes
    βfield: magnification for field imaging between conjugate field plane and reticle plane
    βi: magnification for the intermediate imaging at a single optical element, either for pupil or for field imaging (depending on context)
    R: field radius
    S: working distances
    SEi: working distance with respect to entrance pupil imaging between mirror i on object side
    SEi′: working distance with respect to entrance pupil imaging between mirror i on image side
    SRi: working distance with respect to field imaging between mirror i on object side
    SRi′: working distance with respect to field imaging between mirror i on image side
    eij: distance between optical element i and j
    ωi: angle between incident chief ray and rotation axis of optical element i
    δi: angle between reflected chief ray and rotation axis of optical element i
    a,b,e, ε, p, K: conic section parameters for individual mirror
    di: transversal co-ordinate of intersection point of chief ray with mirror i with respect to rotation axis
    zi: longitudinal co-ordinate of intersection point of chief ray with mirror i with respect to centre of conic section
    βc±: magnification for upper or lower coma or rim rays YDE,
    ZDE: decenter vector components as usual in optical design programs (e.g. CODE V).

## Claims

1. An optical system, comprising:
an illumination system having:
a field plane in which a mask is located;
a conjugated plane, conjugated to said field plane, and having a field stop situated therein, wherein said conjugated plane is situated in a light path from a light source to said field plane, before said field plane, so that light from said light source traverses through said conjugated plane;
a first optical element having a first raster element in said light path before said conjugated plane;
a second optical element having a second raster element in said light path after said first optical element; and
at least a first mirror, in said light path, after said conjugated plane, for imaging a field in said conjugated plane into an image in said field plane.

2. The illumination system of claim 1, further comprising:
a second mirror for imaging said field into said image, wherein light rays travel along a light path from said conjugated plane to said field plane; and
an arc-shaped field in said field plane, whereby said arc-shaped field has a radial direction in a middle of said arc-shaped field defining a scanning direction,
wherein said first mirror and said second mirror are arranged in said light path in such a position and having such a shape, that an edge sharpness of said arc-shaped field is smaller than 5 mm in said scanning direction,
wherein said light rays are impinging on said first mirror and said second mirror with incidence angles less than or equal to 30° or greater than or equal to 60° relative to a surface normal of said first mirror and second mirror.

3. The illumination system according to claim 2, wherein said edge sharpness is smaller than 2 mm.

4. The illumination system according to claim 2, wherein the edge sharpness is smaller than 1 mm.

5. The illumination system according to claim 2, wherein said incidence angles relative to said surface normal are ≦20° or ≧70°.

6. The illumination system according to claim 2, wherein said illumination system includes an object field, and wherein said object field is arc-shaped.

7. The illumination system according to claim 2, wherein said first mirror and said second mirror are part of an imaging system and the imaging system has a magnification ratio unequal to 1.

8. The illumination system according to claim 7, wherein said imaging system is a non-centered system.

9. The illumination system according to claim 2, wherein said first mirror and said second mirror are part of an imaging system and said imaging system comprises an exit pupil and an aperture stop that is located on or close to a plane conjugated to said exit pupil.

10. The illumination system according to claim 2, wherein said first mirror and said second mirror are part of an imaging system, said imaging system comprises an exit pupil, and said first mirror is positioned close to a plane conjugated to the exit pupil.

11. The illumination system according to claim 2, wherein said first mirror and said second mirror are aspheric mirrors.

12. The illumination system according to claim 2, wherein said first mirror is a concave mirror having a nearly hyperbolic form or a nearly elliptic form, and wherein said first mirror defines a first axis of rotation.

13. The illumination system according to claim 12, wherein said second mirror is a concave mirror having a nearly hyperbolic form or a nearly elliptic form, and wherein said second mirror defines a second axis of rotation.

14. The illumination system according to claim 13,
wherein said first axis of rotation and said second axis of rotation subtend to an angle γ, and
wherein said first mirror and said second mirror define a first magnification for a chief array traveling through a center of said field and a center of an exit pupil, a second magnification for an upper COMA ray traveling through said center of the field and an upper edge of said exit pupil and a third magnification for a lower COMA ray traveling through said center of the field and a lower edge of said exit pupil,
whereby the angle γ between said first axis of rotation and said second axis of rotation is chosen so that said first, said second and said third magnification is nearly identical.

15. The illumination system according to claim 2, wherein said first mirror and said second mirror have a used area, and wherein said used area is arranged off-axis with an axis of rotation of said first mirror and said second mirror.

16. The illumination system of claim 2, wherein at least one of said first mirror or said second is an aspheric mirror.

17. The illumination system according to claim 1, further comprising a field-forming optical component in said light path, after said conjugated plane, that shapes said image.

18. The illumination system according to claim 1, further comprising a field-forming optical component in said light path, before said conjugated plane, that forms said field.

19. The illumination system according to claim 17, wherein said field forming optical component is situated in a light path from the light source to said field plane downstream from said conjugated plane to said field plane.

20. The illumination system according to claim 1, wherein said first mirror is part of a multi-mirror system.

21. The illumination system according to claim 1, wherein said first raster element is a field facet and said second raster element is a pupil facet for directing said light from said light source to said conjugated plane.

22. An EUV-projection exposure unit for microlithography, comprising:
the illumination system according to claim 1, wherein said mask is arranged on a carrier system in said field plane; and
a projection objective for imaging said mask onto a light-sensitive object on a carrier system.

23. The EUV-projection exposure unit according to claim 22, wherein the unit is designed as a scanning system.

24. A process for producing microelectronic devices with the EUV-projection exposure unit according to claim 23.

25. The illumination system of claim 1, wherein said source emits light having a wavelength of less than or equal to 193 nm.