1 Introduction
In applications of solar physics, the emission lines of Fe-IX (λ = 17.1 nm), Fe-XII (λ = 19.5 nm), Fe-XV (λ = 28.4 nm) and He-II (λ = 30.4 nm) can be selected as imaging of solar corona 1–9. Due to the strong absorption of most materials in an extreme ultraviolet (EUV) region, the optical system at normal incidence requires a high reflectivity multilayer mirror. In recent years, the achievements in multilayer technology has enabled the development of new instrumentation and led to a number of successful missions such as solar and heliospheric observatory/extreme ultraviolet imaging telescope (SOHO/EIT) and transition region and coronal explorer (TRACE) 1–323. In this article, some multilayer reflective mirrors were studied for He-II radiation (30.4 nm). Usually, at wavelengths longer than the Si L-absorption edge near 12.4 nm, the multilayer material combinations based on Si are widely used in the 13 – 20 nm region 10–151112131416. The Mo/Si multilayer was widely used for its high stability and fairly high reflectivity, especially under the motivation of an EUV lithograph in the integrated circuit industry. However, the reflectivity of a Mo/Si multilayer falls gradually with increasing wavelength. At a wavelength of 30.4 nm, the reflectivity is reduced to about 20%. Therefore, new high-reflectivity multilayer mirrors would have to work at that wavelength. In this paper, reflection performance of some material combinations based on Mg and Si were investigated to design a multilayer at 30.4 nm, including SiC/Mg, B4C/Mg, Mo/Si, B4C/Si, SiC/Si, C/Si, and Sc/Si. Based on optimization of the largest reflectivity and the narrowest width, the SiC/Mg material combination was selected to design the high reflectivity multilayer mirrors for He-II radiation. The multilayers were then prepared by using the direct current magnetron sputtering method, and the reflectivities were measured by the reflectometer at the National Synchrotron Radiation Laboratory (NSRL) in Hefei, China.
2 Design of multilayer mirror
In the EUV region, the closeness of the (real part of the) refractive index, coupled with high absorption, makes the reflectivity of a single layer extremely low, according to the Fresnel formula, with magnitude just in the order of 1 × 10-4. Spiller has proposed that the multilayer film scheme constituted by an absorber and a spacer can improve reflectivity in the region, which essentially means enhancement of multiple-beam interference. To get the highest possible reflectivity of the multilayer, the selection of a material combination should satisfy the following requirements 16,17:
The difference in the real part of the refraction index (n) between the two materials should be the largest.
The absorption at the working wavelength, i.e., the imaginary part of refraction index (k), should be low.
In addition, the interface between the two materials should be smooth and sharp with low diffusion. The n-k complex plane is available for the selection of multilayer materials as shown in
Fig. 1. The optical constants n and k of the materials used at the wavelength of 30.4 nm were shown on a complex plane. It can be seen that the absorption coefficients k of Mg, Si, and Al are lower, and these materials can be selected as space layers in the design. C, SiC, and B4C can be used as absorb layer materials, which also have low absorption and a rather larger difference in the real part of refraction index n. In this paper, some material combinations working at the target wavelength, including Si-based and Mg-based combinations, were calculated for periodical multilayers using a conventional Fresnel theoretical method 18.
Figure 2 shows the calculated reflectivities of different material combinations at an incidence angle of 10° for the wavelength, varying with the bi-layer number. Here, the interface between the materials was considered as an ideal condition, i.e., without roughness and diffusion. It can be seen that the reflectivities of Mg-based material combinations are higher than those of Si-based ones. The Mo/Si combination, which is widely used in the EUV region, has the lowest reflectivity at 30.4 nm (only of 25.61%).
In high-resolution spectroscopy and imaging experiments, a multilayer reflective mirror is required for the highest possible reflectivity and the smallest possible spectral bandwidth (full width at half maximum, FWHM). The calculated peak reflectivities and spectral bandwidths at the wavelength of 30.4 nm and incident angle of 10° are listed in
Tab0 Peak reflectivities and bandwidths(FWHM) at wavelength of 30.4 nm and incident angle of 10° for the 30-pair multilayers shown in Fig. 2 |
| multilayer | layer thickness/nm | reflectivity | Δλ/nm |
|---|---|---|---|
| SiC/Mg | 4.41/11.43 | 0.5603 | 1.67 |
| B4C/Mg | 4.10/11.75 | 0.5816 | 1.83 |
| C/Mg | 4.12/11.73 | 0.5201 | 2.00 |
| C/Al | 4.64/11.93 | 0.3733 | 1.83 |
| C/Si | 5.34/11.63 | 0.2941 | 2.00 |
| SiC/Si | 6.23/10.71 | 0.2648 | 1.50 |
| B4C/Si | 5.93/11.10 | 0.3267 | 2.00 |
| Sc/Si | 3.32/13.34 | 0.2653 | 2.00 |
| Mo/Si | 3.03/13.61 | 0.2561 | 2.33 |
Table 1 for various material combinations with 30-pair multilayers. It can be seen that the SiC/Mg combination has a significantly high reflectivity of 56.03% and narrower bandwidth of 1.67 nm, while the Mo/Si multilayer has a lower reflectivity and the largest bandwidth. The material combination SiC/Mg was thus selected as the multilayer reflective mirror working at the wavelength of 30.4 nm.
3 Preparation and measurement of SiC/Mg multilayer
After design and optimization, the SiC/Mg multilayers were prepared by an ultra-high vacuum direct current magnetron sputtering deposition system (JGP560C6, made in China), which was described in previous article/s 10–151112131415, 17–191819. This system typically reaches a base pressure of about 5 × 10-5 Pa. The working gas is Ar (purity is 99.999%) at the pressure of 0.1 Pa. Deposited multilayers were then measured for quality control and depositing rate control by using a small angle X-ray diffractometer (XRD, D1 system, Bede Ltd, UK). Using the constant power sputtering mode, the deposition rates of Mg and SiC are 0.17 nm/s and 0.10 nm/s, respectively.
Figure 3 shows the XRD measured and fitted results. The period thickness can be calculated from the diffraction peak positions in the measured curve according to the amended Bragg formula. This period thickness is 15.93 nm, which seems a little thicker than the design one (15.84 nm). The fitted data of X-ray diffraction indicates that the thicknesses of Mg and SiC are 11.49 and 4.45 nm respectively 18, which are both thicker than the design ones according to the designed results in Table 1. The value Γ, 0.2791, is the absorber layer thickness ratio of the SiC layer to the period thickness.
The reflective performances of the SiC/Mg multilayers were measured by the reflectometer on beam line U27 at the National Synchrotron Radiation Laboratory (NSRL) in Hefei, China. To suppress high harmonics spectra, an aluminum (A1) filter was inserted into the beam path. Reflectivities were measured at the fixed angle in wavelength-scanning mode.
Figure 4 shows the measured and fitted results of the SiC/Mg multilayer reflective mirror at the design angle (gazing incident angle of 80°). The fitted data in Fig. 4: d = 15.986 nm, γ = 0.2762, σ(SiC/Mg) = 1.834 nm, and σ(Mg/SiC) = 1.916 nm. It can be seen that the peak wavelength is 30.57 nm, deviating from the design one (30.40 nm). After changing the measured grazing incident angle of 78°, the peak reflectivity is 38.0% at the wavelength of 30.36 nm, as shown in
Fig. 5. These synchrotron radiation measured data were also fitted and the results are shown in Figs. 4 and 5. The fitted period thickness (d) and the thickness ratio (γ) coincide with the XRD fitted values shown in Fig. 3. The fitted data in Fig. 5: d = 15.9893 nm, γ = 0.2818, σ(SiC/Mg) = 1.7716 nm, and σ(Mg/SiC) = 1.9389 nm. The fitted results indicate that the roughnesses of SiC_on_Mg interface (σ(SiC/Mg)) and Mg_on_SiC interface (σ(Mg/SiC)) are both about 1.8 nm, which leads to a lower measured reflectivity than the theoretical one. The reflectivity of multilayers is expected to be further increased by reducing interface roughness via optimizing preparation techniques. From Fig. 2 and Table 1, the theoretical reflectivity of a Mo/Si multilayer, which is commonly used in EUV region, can only reach 25.6% at the wavelength of 30.4 nm. Therefore, the reflectivity of the SiC/Mg multilayer prepared by current technique conditions is significantly higher than that of a Mo/Si multilayer.
Calculation and experiment have shown that the SiC/Mg periodical multilayer is a very promising reflective mirror near the wavelength of 30.4 nm. But this multilayer has not yet been extensively studied, especially from the point of view of its thermal stability. Since this mirror will work in the space environment, the thermal stability of an SiC/Mg multilayer is required. A series of annealing experiments were performed in a vacuum chamber at different annealing temperatures for one hour. After annealing, the reflectivities were measured (
Fig. 6). It can be seen that the reflectivity decreases significantly with increasing temperature. When the temperature reaches 500°C, no reflectivity is obtained. Using the electron-induced X-ray emission spectra, we studied the interface of the SiC/Mg multilayer before and after annealing. The measurements were performed by Mg–Kβ and Si–Kβ, respectively 20. Both of the measured results show that Mg reacts with Si to form Mg2Si at the interface of the multilayer. Thus, the barrier layer at the interfaces will be inserted to enhance the thermal stability of the SiC/Mg multilayer.
4 Summary
For the extreme ultraviolet imaging of solar corona by selecting an He-II emission line, a promising SiC/Mg multilayer reflective mirror was designed, prepared and measured. At the grazing incident angle of 78°, the measured reflectivity is 38.0% at the wavelength of 30.4 nm. However, the difference between theoretical reflectivity and measured reflectivity indicates significant roughness on the multilayer interface. The annealing experiment suggests that the thermal stability is weak. Further investigation on the design and fabrication technology is required.