Abstract:
An optical system of a high-resolution imaging spectrograph intended for deep ultraviolet Raman spectroscopy, including an entrance aperture constituted by a slit, followed by a collimating objective, with a dispersive element located between the collimating objective and the subsequent focusing objective is provided. A multichannel radiation detector is arranged behind the focusing objective. The collimating objective is formed at least by a main mirror, wherein the focussing objective is formed by a set of lenses. The dispersion element is formed at least by one diffraction grating  4  and/or an optical prism.

Description:
CROSS-REFERENCE TO RELATED APPLICATIONS 
       [0001]    This application claims priority to Czech Application No. PV 2014-882, having a filing date of Dec. 10, 2014, the entire contents of which are hereby incorporated by reference. 
       FIELD OF TECHNOLOGY 
       [0002]    The following relates to an arrangement of an optical system of a high lens speed, high-resolution imaging spectrograph to detect the electromagnetic spectrum that is primarily intended for ultraviolet Raman spectroscopy, in particular for identification of substances in determining their composition and structure, and for analysis of surfaces and biological systems. 
       BACKGROUND 
       [0003]    At present, spectrographs containing basic optical elements are mainly used to detect the incident electromagnetic radiation differentiated according to wavelengths, such basic optical elements being: an aperture for the entering polychromatic, usually divergent radiation beam, e.g. a slit. Furthermore, a collimating element which converts the divergent optical beam coming from the entrance aperture into a collimated beam—which is parallel. Further, a dispersive element, generally an element causing refractive dispersion (light refraction) or diffractive dispersion (light diffraction) of a polychromatic beam into monochromatic beams according to wavelengths. Further, it comprises a focusing element, which generates an image of the entrance aperture—usually a slit, at the site of a certain focal plane of the exit aperture, usually on the flat multi-channel radiation detector, in order to record simultaneously the radiation of a large number of wavelengths. The dispersive element in multi-channel detectors is usually a diffraction grating or a dispersive prism. 
         [0004]    Notes on Raman spectroscopy: Raman spectroscopy is used to study the structure of Raman scattering molecules. Raman scattering is an inelastic scattering of the optical radiation on the molecules of the test substance, at which the frequency of the scattered radiation is shifted towards the frequency of the incident radiation by a value that corresponds to the rotational or vibrational transition in the molecule. A molecule can exist in states with energy that acquires only certain allowed values or energy levels. Vibrational or rotational transition is a change in the molecular state characterized by an abrupt change in the vibrational and rotational energy levels of the molecule. Vibrational energy level is a possible value of energy that is acquired by a molecule in the vibrational motion of its atoms around their equilibrium position. Rotational energy level is a value of energy that can be acquired by a molecule during its rotational movement around the axis passing through its center of gravity. These energy levels are dependent on the particular atomic structure and their spatial arrangement, i.e. on the type of the test substance. 
         [0005]    Raman spectroscopy is used to measure inelastically scattered light (Raman scattering) on the molecules of the test substance. Scattered radiation has a different wavelength than the incident radiation, due to interactions of the radiation with vibrational and in some cases rotational states of molecules. The scattered radiation carries a large amount of information about the nature and structure of the test substance. Resonance enhancement of Raman scattering of biologically relevant substances (proteins, nucleic acids, and others) can be achieved in the ultraviolet region of the spectrum, at about 205 to 270 nm, to obtain additional unique information on these substances. 
         [0006]    Raman scattering is a relatively weak phenomenon. The spectrograph for Raman spectroscopy is subject to high demands in terms of lens speed, i.e. the amount of radiation transferred to the detector. Further efforts are needed to achieve high resolution (0.03 to 0.06 nm) and spectral range of tens of nanometers. 
         [0007]    The currently used and commercially available spectrographs (supplied by Horiba Jobin Yvon, Princeton Instruments, Andor) useful for Raman scattering in the UV region, are generally composed of two mirrors and a reflective diffraction grating. Alternatively, the optical assembly is complemented by an additional correction mirror, as described for example in the U.S. Patent Publication 2013/0182250 A1. The patent covers the design of mirror imaging spectrographs, in which the assembly of the collimating mirror, diffraction grating and focusing mirror is supplemented by at least one corrective aspheric mirror, which is intended to correct extra-axial imaging defects (aberrations), in particular astigmatism and coma. The advantage of the mirror systems is their achromaticity (absence of color defects) and a relatively high reflectivity. The disadvantages are the limited possibility of correction of other optical defects, in particular astigmatism and coma. Moreover, these spectrographs achieve maximum lens speed of only about f/4. 
         [0008]    Better correction of optical defects, and thereby a higher lens speed, can be achieved using lens objectives. In the visible spectral range, these systems with the lens speed of up to f/1.8 and using transmission gratings (supplied by Kaiser, model Holospec f/1.8) are very well available. However, the situation in the ultraviolet spectral region is completely different, mainly due to the limited number of transparent optical materials. There is high demand on the design of lenses, thus increasing the complexity of the system and its cost. The scientific literature describes only one spectrograph operating in the UV spectral region and containing lens objectives as collimating and focusing elements, which achieves the nominal lens speed of f/2. This system, however, achieves spectral resolution of only 12-14 cm −1  and its throughput is limited by surface losses and vignetting (blocking of the outer parts of the beam) due to a large distance between the collimating and focusing objectives. 
       SUMMARY 
       [0009]    An aspect relates to a spectrograph that achieves a higher lens speed (f/2) than the mirror systems, while maintaining high spectral resolution necessary for Raman spectroscopy, and achieving a higher throughput than that of the full lens system. The spectrograph should be applicable for multichannel detectors equipped with a cooled detector chip and a cover glass. It requires the use of a circular pupil of the focusing aspect for the diffracted radiation beam. The system must allow tuning, i.e., a change in the wavelength range by simply rotating the diffraction grating, and a small change in the position and orientation of the detector—focusing into the focusing plane. 
         [0010]    The said goal is largely met by the high resolution imaging spectrograph, intended for deep ultraviolet Raman spectroscopy, the optical system of which comprises an entrance aperture formed by a slit, which is followed by a collimating objective, with a dispersive element placed between the collimating objective and the focusing objective, and a multi-channel radiation detector behind the focusing objective. Embodiments of the invention are characterized in that the collimating aspect is formed by at least a main mirror, while the said focusing aspect is formed by a set of lenses. At the same time, the dispersive element is formed by at least one diffraction grating and/or an optical prism. 
         [0011]    The optical system of the imaging spectrograph may have a collimating aspect comprising an aspherical mirror and a corrective mirror with an aperture. 
         [0012]    In a preferable embodiment, the focusing aspect consists of seven lenses, of which at least one has an aspherical surface. 
         [0013]    The higher performance of the spectrograph with an optical system as per embodiments of the invention is that it achieves a higher lens speed (f/2) than the mirror systems, while maintaining high spectral resolution required for Raman spectroscopy. It also achieves a higher throughput than that of the full lens system. The spectrograph can be used with multi-channel detectors equipped with a cooled detector chip and a glass cover. It is advantageous to use the circular pupil of the focusing aspect for the diffracted radiation beam. Embodiments of the invention must allow tuning, e.g., a change in the wavelength range by simply rotating the diffraction grating, and a small change in the position and orientation of the detector—focusing into the focusing plane. 
     
    
     
       BRIEF DESCRIPTION 
         [0014]    Some of the embodiments will be described in detail, with reference to the following figures, wherein like designations denote like members, wherein: 
           [0015]      FIG. 1  is an embodiment of the collimating objective formed by a pair of mirrors with a diffraction grating and a seven-lens focusing objective. 
           [0016]      FIG. 2  is a simplified embodiment of the diffraction grating as a dispersive element, wherein the focusing objective is formed by one mirror, 
           [0017]      FIG. 3  shows an example of embodiment with a pair of mirrors in the collimating objective and an assembly of five lenses in the focusing objective, 
           [0018]      FIG. 4  shows an example of embodiment wherein the dispersion of polychromatic beam is achieved by a dispersive system consisting of a combination of grating and prism. 
       
    
    
     DETAILED DESCRIPTION 
     Example 1 
       [0019]    Collimating objective  7  of the spectrograph, the optical system of which is shown in  FIG. 1 , consists of two aspherical mirrors  2 ,  3 , designated as main  2  and corrective  3 . The aspherical corrective mirror  3  has an aperture  10  in its center, with size allowing passage of the polychromatic divergent light beam  11  originating from slit  1  without being vignetted at the edges. The focusing objective  8  consists of the assembly  9  of seven lenses  9 . 1 ,  9 . 2 ,  9 . 3 ,  9 . 4 ,  9 . 5 ,  9 . 6 ,  9 . 7 , one of them having an aspherical surface. A combination of fused silica and CaF 2  has been selected as the material of the individual optical elements of the focusing objective  8 . Diffraction grating  4  with a frequency of 3600 lines/mm is placed between the collimating objective  7  and the focusing objective  8 . The diffraction grating  4  uses the first diffraction order, with &gt;40% efficiency. Before hitting the detector  6 , the light beam  11  passes through the cover glass  5  which is a part of detector  6 . Parameters of the respective optical surfaces are shown below in Table 1. 
         [0020]    Aspherical surface is defined by the relation 
         [0000]    
       
         
           
             z 
             = 
             
               
                 
                   cr 
                   2 
                 
                 
                   1 
                   + 
                   
                     
                       1 
                       - 
                       
                         
                           ( 
                           
                             1 
                             + 
                             K 
                           
                           ) 
                         
                          
                         
                           c 
                           2 
                         
                          
                         
                           r 
                           2 
                         
                       
                     
                   
                 
               
               + 
               
                 
                   ∑ 
                   i 
                 
                  
                 
                   
                     A 
                     i 
                   
                    
                   
                     r 
                     i 
                   
                 
               
             
           
         
       
     
         [0000]    where c is the surface curvature (the reciprocal value of the radius), K is the conic constant, r is the radial coordinate and Ai are aspherical coefficients. 
         [0021]    Parameters of the respective optical media a through q of the optical system according to  FIG. 1  are shown in Table 1, where the dimensions are given in mm. 
         [0000]    
       
         
               
             
               
               
               
               
               
             
               
               
               
               
               
             
           
               
                 TABLE 1 
               
             
             
               
                   
               
               
                 Parameters of the spectrograph as per FIG. 1 
               
               
                 Example 1 of the invention application 
               
               
                 (dimensions in mm) 
               
             
          
           
               
                 area 
                 radius 
                 thickness 
                 material 
                 comments 
               
               
                   
               
             
          
           
               
                 1 
                 plane 
                 200 
                 air 
                 Slit 1 
               
               
                 a 
                 401.789 
                 −180 
                 mirror 
                 Main aspherical mirror 2 
               
               
                   
                   
                   
                   
                 K = 0.107497, A4 = −1.572858E−9, 
               
               
                   
                   
                   
                   
                 A6 = −1.006896E−13, A 8  = 1.991723E−17, 
               
               
                   
                   
                   
                   
                 A10 = −1.855797E−21 
               
               
                 b 
                 93476.4 
                 200 
                 mirror 
                 Correction aspherical mirror 3 
               
               
                   
                   
                   
                   
                 K = −4995714, A4 = −2.348767E−9, 
               
               
                   
                   
                   
                   
                 A6 = −2.497952E−13, A 8  = 4.020043E−17, 
               
               
                   
                   
                   
                   
                 A10 = −3.148018E−21 rotated by 20°; 
               
               
                 c 
                 plane 
                 80 
                 mirror 
                 diffraction grating 4 with frequency of 3600 
               
               
                   
                   
                   
                   
                 lines/mm; rotated by −0.7° (for the wavelength 
               
               
                   
                   
                   
                   
                 range from 250 to 272 nm) 
               
               
                   
                   
                   
                   
                 the angle between the optical axes of lenses 7, 8 = 
               
               
                   
                   
                   
                   
                 68° 
               
               
                 d 
                 224.497 
                 −6.293 
                 fused silica 
                 lens 9.1 
               
               
                 e 
                 182.502 
                 −8.242 
                 air 
               
               
                 f 
                 57.558 
                 −20.004 
                 fused silica 
                 lens 9.2 
               
               
                 g 
                 −93.609 
                 −0.296 
                 air 
               
               
                 h 
                 −63.458 
                 −16.898 
                 CaF 2   
                 lens 9.3 
               
               
                 i 
                 68.974 
                 −0.175 
                 air 
               
               
                 j 
                 107.435 
                 −10.172 
                 CaF 2   
                 lens 9.4 
               
               
                 k 
                 97.214 
                 −6.266 
                 air 
               
               
                 l 
                 51.565 
                 −4.987 
                 fused silica 
                 lens 9.5 
               
               
                 m 
                 −41.336 
                 −0.619 
                 air 
               
               
                 n 
                 −42.117 
                 −20.034 
                 CaF 2   
                 lens 9.6 
               
               
                 o 
                 72.268 
                 −42.402 
                 air 
               
               
                 p 
                 −52.762 
                 −18.005 
                 fused silica 
                 Lens 9.7 
               
               
                   
                   
                   
                   
                 K = −15.14056, A4 = −9.654539E−6, 
               
               
                   
                   
                   
                   
                 A6 = 2.199664E−8, A 8  = −1.537923E−11 
               
               
                 q 
                 −28.218 
                 −8.772 
                 air 
               
               
                 r 
                 plane 
                 −1 
                 fused silica 
                 cover glass 5 
               
               
                 s 
                 plane 
                 −9 
                 air 
               
               
                 image 
                 plane 
                   
                   
                 detector 6 
               
               
                   
               
               
                 *Where K denotes conicity and A i  other aspheric coefficients 
               
             
          
         
       
     
       Example 2 
       [0022]    The collimating objective  7  of the spectrograph, the optical system of which is shown in  FIG. 2 , unlike the previous embodiment example, consists of the off-axis, biconic, aspherical mirror  2 . The focusing objective  8  consists of seven lenses  9 . 1 ,  9 . 2 ,  9 . 3 ,  9 . 4 ,  9 . 5 ,  9 . 6 , and  9 . 7 . A combination of fused silica and CaF 2  has been selected as the material of the individual optical elements of the focusing objective  8 . Diffraction grating  4  with a frequency of 3600 lines/mm is placed between the collimating objective  7  and the focusing objective  8 . The diffraction grating  4  uses the first diffraction order, with &gt;40% efficiency. The polychromatic divergent light beam coming out of the slit  1  falls on the collimating objective  7  consisting of one main mirror  2  and is reflected to the diffraction grating  4 . Diffraction of the light beam occurs on the diffraction grating  4  dispersing the polychromatic beam due to the effects of light diffraction on the grating  4 . Before hitting the detector  5 , the light beam may or may not pass through the cover glass  4  which is a part of detector  6 . Parameters of the respective optical surfaces in this particular embodiment are specified below in Table 2. 
         [0000]    
       
         
               
             
               
               
               
               
               
             
               
               
               
               
               
             
           
               
                 TABLE 2 
               
             
             
               
                   
               
               
                 Parameters of the spectrograph as per FIG. 2 
               
               
                 Example 2 of the invention application 
               
               
                 (dimensions in mm) 
               
             
          
           
               
                 area 
                 radius 
                 thickness 
                 material 
                 comments 
               
               
                   
               
             
          
           
               
                 object 
                 plane 
                 200 
                 air 
                 Slit 1 
               
               
                 a 
                 * 
                 −190 
                 Mirror 
                 Mirror 2 biconic surface 
               
               
                   
                   
                   
                   
                 * . . . radius r1 = −400.023; K1 = −0.999427 radius 
               
               
                   
                   
                   
                   
                 r 2  (perpendicular to r1) = −400.370; 
               
               
                   
                   
                   
                   
                 K 2  = −0.998466 
               
               
                 b 
                 plane 
                 80 
                 mirror 
                 diffraction grating 4 with a frequency of 3600 
               
               
                   
                   
                   
                   
                 lines/mm 
               
               
                   
                   
                   
                   
                 rotated by −6.88° (for the wavelength range from 
               
               
                   
                   
                   
                   
                 205 to 220 nm) 
               
               
                   
                   
                   
                   
                 the angle between the beam incident on the 
               
               
                   
                   
                   
                   
                 diffraction grating 4 and the optical axis of the 
               
               
                   
                   
                   
                   
                 focusing objective 8 is 68 degrees 
               
               
                 c 
                 77.288 
                 5.977 
                 fused silica 
                 lens 9.1 
               
               
                 d 
                 233.929 
                 7.676 
                 air 
               
               
                 e 
                 −84.931 
                 20.012 
                 fused silica 
                 lens 9.2 
               
               
                 f 
                 64.985 
                 1.869 
                 air 
               
               
                 g 
                 54.381 
                 25.005 
                 CaF 2   
                 lens 9.3 
               
               
                 h 
                 −85.406 
                 0.181 
                 air 
               
               
                 i 
                 115.500 
                 10.081 
                 CaF 2   
                 lens 9.4 
               
               
                 
                   j 
                 
                 −93.643 
                 5.606 
                 air 
               
               
                 k 
                 −54.296 
                 15.016 
                 fused silica 
                 lens 9.5 
               
               
                 l 
                 42.624 
                 3.859 
                 air 
               
               
                 m 
                 49.866 
                 20.015 
                 CaF 2   
                 lens 9.6 
               
               
                 n 
                 −76.024 
                 45.024 
                 air 
               
               
                 o 
                 34.906 
                 18.024 
                 fused silica 
                 lens 9.7 
               
               
                 p 
                 26.760 
                 10.022 
                 air 
               
               
                 q 
                 plane 
                 1 
                 fused silica 
                 cover glass 5 
               
               
                 r 
                 plane 
                 9 
                 air 
               
               
                 image 
                 plane 
                   
                   
                 detector 6 
               
               
                   
               
               
                 * Where K i  denotes conicity 
               
             
          
         
       
     
         [0023]    The beam incident on the focusing objective  8  has a circular cross section, while the beam coming out of the collimating objective  7  and incident on the diffraction grating  4  has an elliptical cross section. 
       Example 3 
       [0024]    The embodiment example 3 differs from example 1 in that the focusing objective  8  is composed of five lenses  9 . 1 ,  9 . 2 ,  9 . 3 ,  9 . 4  and  9 . 5 . 
         [0025]    Collimating objective  7  of the spectrograph, the optical system of which is shown in  FIG. 3 , consists of two aspherical mirrors  2 ,  3 , which are designated as main mirror  3  and corrective mirror  2 . The aspherical corrective mirror  3  has an aperture  10  in its center, with size allowing passage of the polychromatic divergent light beam coming out of the slit  1 , without being vignetted at the edges. The focusing objective  8  is composed of five lenses  9 . 1 ,  9 . 2 ,  93 ,  9 A, and  9 . 5 , three of them having aspherical surfaces. A combination of fused silica and CaF 2  has been selected as the material of the individual optical elements of the focusing objective  8 . Diffraction grating  4  with a frequency of 3600 lines/mm is placed between the collimating objective  7  and the focusing objective  8 . The grating  4  uses the first diffraction order, with &gt;40% efficiency. Before hitting detector  6 , the light beam may pass through the cover glass  5 , which is a part of detector  6 . Parameters of the respective optical surfaces are shown below in Table 3. Aspherical surface is defined by the relation (A). Parameters of the respective optical media a through o of the optical system according to  FIG. 2  are shown in Table 2, where the dimensions are given in mm. 
         [0000]    
       
         
               
             
               
               
               
               
               
             
               
               
               
               
               
             
           
               
                 TABLE 3 
               
             
             
               
                   
               
               
                 Parameters of example 3 of the spectrograph embodiment: 
               
               
                 Example 3 of the invention application 
               
               
                 (dimensions in mm) 
               
             
          
           
               
                 area 
                 radius 
                 thickness 
                 material 
                 comments 
               
               
                   
               
             
          
           
               
                 object 
                 plane 
                 200 
                 air 
                 Slit 4 
               
               
                 a 
                 −401.79 
                 −180 
                 mirror 
                 Main mirror 2, * K = 0.107491, A 4  = −1.572926E−9, 
               
               
                   
                   
                   
                   
                 A 6  = −1.006967E−13, A 8  = 1.991713E−17, 
               
               
                   
                   
                   
                   
                 A 10  = −1.844422E−21 
               
               
                 b 
                 93664.6 
                 200 
                 mirror 
                 Correction mirror 3, rotated by 20 degrees; 
               
               
                   
                   
                   
                   
                 K = −4995723, A 4  = −2.342046E−9, A 6  = −2.501973E−13 
               
               
                   
                   
                   
                   
                 A 8  = 4.018759E−17 A 10  = −3.162602E−21 
               
               
                 c 
                 plane 
                 −80 
                 mirror 
                 diffraction grating 4 with the frequency of 3600 
               
               
                   
                   
                   
                   
                 lines/mm; rotated by −2.7° (for the wavelength 
               
               
                   
                   
                   
                   
                 range from 218 to 234 nm) 
               
               
                   
                   
                   
                   
                 the angle between the beam incident on the 
               
               
                   
                   
                   
                   
                 diffraction grating 4 and the optical axis of the 
               
               
                   
                   
                   
                   
                 focusing objective 8 is 68 degrees 
               
               
                 d 
                 −72.079 
                 −3.000 
                 fused silica 
                 lens 9.1 
               
               
                 e 
                 −41.655 
                 −1.000 
                 air 
               
               
                 f 
                 −36.205 
                 −18.125 
                 fused silica 
                 lens 9.2 
               
               
                   
                   
                   
                   
                 K = −0.011368, A 4  = 3.305605E−7, 
               
               
                   
                   
                   
                   
                 A 6  = 2.311898E−9, A 8  = −7.310637E−13 
               
               
                 g 
                 70.164 
                 −4.099 
                 air 
               
               
                 h 
                 54.186 
                 −3.275 
                 CaF 2   
                 lens 9.3 
               
               
                 i 
                 −37.146 
                 −0.498 
                 air 
               
               
                 j 
                 −37.695 
                 −20.002 
                 CaF 2   
                 lens 9.4 
               
               
                 k 
                 75.983 
                 −39.398 
                 air 
                 K = −0.619901, A 4  = 7.664860E−7, 
               
               
                   
                   
                   
                   
                 A 6  = 2.173671E−9, A 8  = −3.028988E−12 
               
               
                 l 
                 −59.329 
                 −20.000 
                 fused silica 
                 lens 9.5 
               
               
                   
                   
                   
                   
                 K = −2.313735, A 4  = 4.698205E−7, 
               
               
                   
                   
                   
                   
                 A 6  = 1.901152E−8, A 8  = −2.225080E−11 
               
               
                 m 
                 −36.803 
                 −10.314 
                 air 
               
               
                 n 
                 plane 
                 −1 
                 fused silica 
                 cover glass 5 
               
               
                 o 
                 plane 
                 −9 
                 air 
               
               
                 image 
                 plane 
                   
                   
                 detector 6 
               
               
                   
               
               
                 * Where K denotes conicity and A i  other aspheric coefficients 
               
             
          
         
       
     
       Example 4 
       [0026]    Embodiment example 4, according to  FIG. 4 , is different compared to the embodiment 1 in that it comprises in addition a dispersive prism  41  in the optical assembly. The optical prism  41  has two functions: it increases the spectral resolution by increasing the total dispersion of the system, and it compensates for beam expansion (anamorphic reduction) on the diffraction grating  4 , so that the collimated beam incident on and coming out of the system of dispersive elements  41 ,  4  has about a circular cross section. 
         [0027]    Collimating objective  7  of the spectrograph, the optical system of which is shown in  FIG. 4 , consists of two aspherical mirrors  2 ,  3 , which are designated as main mirror  3  and corrective mirror  2 . The aspherical corrective mirror  3  has an aperture  10  in its center, with size allowing passage of the polychromatic divergent light beam coming out of the slit  1 , without being vignetted at the edges. The focusing objective  8  consists of the set of seven lenses  9 . 1 ,  9 . 2 ,  9 . 3 ,  9 . 4 ,  9 . 5 ,  9 . 6 , and  9 . 7 , one of them having an aspherical surface. A combination of fused silica and CaF 2  has been selected as the material of the individual optical elements of the focusing objective  8 . A combination of prism  41  and diffraction grating  4  with a frequency of 3600 lines/mm is placed as a dispersive element between the collimating objective and the focusing objective. The grating  4  uses the first diffraction order, with &gt;40% efficiency. Before hitting detector  7 , the light beam may pass through the cover glass  5  which is a part of detector  6 . Parameters of the respective optical surfaces are shown below in Table 4. 
         [0028]    Aspherical surface is defined by the relation 
         [0000]    
       
         
           
             z 
             = 
             
               
                 
                   cr 
                   2 
                 
                 
                   1 
                   + 
                   
                     
                       1 
                       - 
                       
                         
                           ( 
                           
                             1 
                             + 
                             K 
                           
                           ) 
                         
                          
                         
                           c 
                           2 
                         
                          
                         
                           r 
                           2 
                         
                       
                     
                   
                 
               
               + 
               
                 
                   ∑ 
                   i 
                 
                  
                 
                   
                     A 
                     i 
                   
                    
                   
                     r 
                     i 
                   
                 
               
             
           
         
       
     
         [0029]    Parameters of the respective optical media a through u of the optical system according to  FIG. 4  are shown in Table 4, where the dimensions are given in mm. 
         [0000]    
       
         
               
             
               
               
               
               
               
             
           
               
                 TABLE 4 
               
             
             
               
                   
               
               
                 Parameters of example 4 of the spectrograph embodiment: 
               
               
                 Example 4 of the invention application 
               
               
                 (dimensions in mm) 
               
             
          
           
               
                 area 
                 radius 
                 thickness 
                 material 
                 comments 
               
               
                   
               
               
                 object 
                 plane 
                 200    
                 air 
                 Slit 4 
               
               
                 a 
                 −401.79 
                 −180     
                 mirror 
                 Main mirror 2, K = 0.107491, A 4  = − 1.572926E−9, 
               
               
                   
                   
                   
                   
                 A 6  = −1.006967E−13, A 8  = 1.991713E−17, 
               
               
                   
                   
                   
                   
                 A 10  = −1.844422E−21 
               
               
                 b 
                 93664.6 
                 300    
                 mirror 
                 Correction mirror 3, rotated by 20 degrees; 
               
               
                   
                   
                   
                   
                 K = −4995723, A 4  = −2.342046E−9, A 6  = −2.501973E−13 
               
               
                   
                   
                   
                   
                 A 8  = 4.018759E−17 A 10  = −3.162602E−21 
               
               
                 c 
                 plane 
                 35 *  
                 fused silica 
                 Prism 41, - Angle of rotation 56.38°. 
               
               
                   
                   
                   
                   
                 Apex angle of 18°. 
               
               
                 d 
                 plane 
                 169.26  
                 air 
               
               
                 e 
                 plane 
                 −90    
                 mirror 
                 diffraction grating 4 with the frequency of 3600 
               
               
                   
                   
                   
                   
                 lines/mm; rotated by −3.5° (for the wavelength 
               
               
                   
                   
                   
                   
                 range from 218 to 234 nm) 
               
               
                   
                   
                   
                   
                 the angle between the beam incident on the 
               
               
                   
                   
                   
                   
                 diffraction grating 4 and the optical axis of the 
               
               
                   
                   
                   
                   
                 focusing objective 8 is 68 degrees 
               
               
                 f 
                 — 
                 −9.511 
                 fused 
                 Lens 9.1 
               
               
                   
                 224.724 
                   
                 silica 
               
               
                 g 
                 182.405 
                 −9.187 
                 air 
               
               
                 h 
                 57.466 
                 −18.616  
                 fused silica 
                 lens 9.2 
               
               
                 i 
                 −94.675 
                 −0.515 
                 air 
               
               
                 
                   j 
                 
                 −63.907 
                 −16.996  
                 CaF 2   
                 lens 9.3 
               
               
                 k 
                 68.392 
                 −0.158 
                 air 
               
               
                 l 
                 108.433 
                 −10.276  
                 CaF 2   
                 lens 9.4 
               
               
                 m 
                 95.827 
                 −6.298 
                 air 
               
               
                 n 
                 51.242 
                 −6.647 
                 fused silica 
                 lens 9.5 
               
               
                 o 
                 −41.349 
                 −0.977 
                 air 
               
               
                 p 
                 −42.500 
                 −20.147  
                 CaF 2   
                 lens 9.6 
               
               
                 q 
                 71.780 
                 −42.226  
                 air 
               
               
                 r 
                 −56.418 
                 −17.998  
                 fused silica 
                 lens 9.7 
               
               
                   
                   
                   
                   
                 K = −15.31897, A 4  = −7.803339E−6, 
               
               
                   
                   
                   
                   
                 A 6  = 1.732514E−8, A 8  = −1.043447E−11 
               
               
                 s 
                 −31.282 
                 −8.077 
                 air 
               
               
                 t 
                 plane 
                 −1    
                 fused silica 
                 cover glass 5 
               
               
                 u 
                 plane 
                 −9    
                 air 
               
               
                 image 
                 plane 
                   
                   
                 detector 6 
               
               
                   
               
               
                 * Where K denotes conicity and A i  other aspheric coefficients 
               
             
          
         
       
     
         [0030]    Other parameters common to all embodiment examples: 
         [0000]    Lens speed of the spectrograph: at least f/2
 
The focal length of the focusing objective  8 : 100 mm
 
Resolution of lenses  7 ,  8 : 40 lines per mm
 
The absolute value of magnification of the optical system: 0.5×
 
         [0031]    The spectrograph is intended for multichannel cooled detectors  6  with the following parameters:
       the size of the visible field at least 15×6 mm   pixel size: 13×13 um to 26×26 um   cover glass  5  of fused silica with thickness 0-1.5 mm       
 
         [0035]    The spectral resolution of the spectrograph is dependent on the selected spectral range (excitation wavelength), and is shown in Table 5 for the aforementioned embodiment example 1: 
         [0000]    
       
         
               
             
               
               
               
               
             
               
               
               
               
               
               
             
               
               
               
               
               
               
             
           
               
                 TABLE 5 
               
             
             
               
                   
               
               
                 Spectral resolution for the various spectrograph configurations 
               
             
          
           
               
                   
                 Wavelength 
                 Angle 
                   
               
               
                   
                 excitation 
                 rotation of 
                   
               
               
                   
                 length 
                 grating 4 
                 Spectral resolution (cm −1 ) 
               
             
          
           
               
                 Config. 
                 (nm) 
                 (deg) 
                 500 cm −1   
                 1800 cm −1   
                 3200 cm −1   
               
               
                   
               
             
          
           
               
                 1 
                 250 
                 −0.7 
                 8.9 
                 7.1 
                 4.4 
               
               
                 2 
                 240 
                 1.0 
                 9.9 
                 8.2 
                 5.7 
               
               
                 3 
                 230 
                 2.7 
                 11.3 
                 9.4 
                 7.0 
               
               
                 4 
                 218 
                 4.4 
                 13.0 
                 11.0 
                 9.0 
               
               
                 5 
                 205 
                 6.5 
                 14.9 
                 13.3 
                 11.3 
               
               
                   
               
             
          
         
       
     
         [0036]    Embodiments of the invention need not be limited to these examples. In practice, values of the individual parameters of the focusing objective  8  may range in the following intervals: 
         [0000]    
       
         
               
             
               
               
               
               
             
           
               
                 TABLE 6 
               
             
             
               
                   
               
               
                 Possible range of parameters for the focusing objective 8 
               
               
                 Range of parameters for the focusing objective 8 
               
               
                 (dimensions in mm) 
               
             
          
           
               
                 radius 
                 thickness 
                 material 
                 comments 
               
               
                   
               
               
                 −210 ÷ −230 (convex) 
                  −5 ÷ −10 
                 fused silica 
                 lens 9.1 
               
               
                 180 ÷ 190 (convex) 
                  −7 ÷ −10 
                 air 
               
               
                     55 ÷ 58 (concave) 
                  −7 ÷ −20 
                 fused silica 
                 lens 9.2 
               
               
                     −90 ÷ −100 (concave) 
                 −0.25 ÷ −0.5  
                 air 
               
               
                 −60 ÷ −65 (convex) 
                 −15 ÷ −20 
                 CaF2 
                 lens 9.3 
               
               
                 65 ÷ 75 (convex) 
                 −0.15 ÷ 0.2  
                 air 
               
               
                 −100 ÷ −110 (convex) 
                 −10 ÷ −12 
                 CaF2 
                 lens 9.4 
               
               
                  80 ÷ 100 (convex) 
                 −4 ÷ −7 
                 air 
               
               
                     50 ÷ 55 (concave) 
                  −5 ÷ −15 
                 fused silica 
                 lens 9.5 
               
               
                     −35 ÷ −45 (concave) 
                 −0.5 ÷ −2     
                 air 
               
               
                 −40 ÷ −45 (convex) 
                 −20 ÷ −25 
                 CaF2 
                 lens 9.6 
               
               
                 70 ÷ 75 (convex) 
                 −35 ÷ −45 
                 air 
               
               
                 50 ÷ 65 (convex) 
                 −17 ÷ −19 
                 fused silica 
                 lens 9.7 
               
               
                   
                   
                   
                 K = −15 ÷ −20 
               
               
                   
                   
                   
                 A 4  = −6 ÷ −10E−6 
               
               
                   
                   
                   
                 A 6  = 1.5 ÷ 2.5E−8 
               
               
                   
                   
                   
                 A 8  = −1 ÷ −1.6E−11 
               
               
                     −25 ÷ −35 (concave) 
                  −7 ÷ −10 
                 air 
               
               
                   
               
               
                 Where K denotes conicity and A i  other aspheric coefficients 
               
             
          
         
       
     
         [0037]    The function of the optical system according to embodiments of the invention, i.e. the spectrograph function according to examples 1 and 3 is as follows: 
         [0038]    The polychromatic divergent light beam enters into the spectrograph system through the slit  1 , passes through the aperture  10  in the aspherical correction mirror  3  and falls on the main correction mirror  2 , from which it is reflected. Given the shape of the main correction mirror  2  and the fact that the slit  1  is close to its focal point, the divergent beam becomes almost collimated after the reflection. The beam continues to the aspherical correction mirror  3 , from which it is also reflected, and due to the influence of the aspherical surface, the beam becomes even more collimated. The collimated beam then falls on the reflective diffraction grating  4 . Upon incidence on the grating  4  the light beam is diffracted and the polychromatic beam is diffracted on the grating  4  to the respective monochromatic beams which are then further spread under different angles corresponding to their wavelengths. These beams pass through the seven-lens focusing objective  8 , which is intended to focus the beams onto the detector  6 . Before hitting detector  6  the beams pass through the glass cover  5 , which serves as a protection of detector  6 . 
       INDUSTRIAL APPLICABILITY 
       [0039]    The embodiments of the invention can be applied in high-resolution imaging spectrographs for deep UV Raman spectroscopy. Spectrographs with the applied invention can be produced in an industrial scale.