1.
Introduction
High-sensitivity X-ray detectors are affected by out-of-range radiation [microwave, infrared (IR), visible (VIS), and ultraviolet (UV)], which can deteriorate their performance. The presence of filters to shield the detectors is thus necessary for the correct operation of the detector, yet their X-ray transparency must be maximized to guarantee a high detection efficiency.
Charge-coupled devices, silicon drift detectors, and depleted p-channel field effect transistor arrays, as baselined for the wide field imager1 (WFI) instrument of the Athena mission, are sensitive to UV and visible photons with energy larger than the Si band gap. If these photons hit such a detector, electron-hole pairs are formed, which add to those generated by the X-ray photon, causing a spectral resolution degradation, and a shift of the energy scale by a few eV. An optical blocking filter (OBF) is thus required to remove UV and visible radiation which is typically brighter than X-rays in most astrophysical sources.2 OBFs are particularly important for experiments observing the EUV and X-ray emission from the chromosphere and solar corona, in this case the much brighter UV/VIS emission from the photosphere must be fully blocked. A few such examples include the X-ray telescope experiment3 on Hinode, the extreme ultraviolet imaging telescope4 experiment on Solar and Heliospheric Observatory, and the extreme ultraviolet imager experiment5 on Solar Orbiter.
Filters are usually made of a shielding layer, usually a low-Z metal such as aluminum for keeping a low X-ray attenuation, and a supporting membrane, which is needed because the low thickness needed to allow for limiting the X-ray attenuation does not ensure sufficient mechanical strength.
Silicon nitride is a good candidate as a filter support material since both silicon and nitrogen are low-Z chemical elements, silicon nitride (SiN) is known to be thermodynamically stable 6 ,7 and, additionally, the related technological processes are well developed because this compound is extensively employed in the fabrication of integrated circuits. The most used materials to fabricate filters for X-rays missions are polymers, in particular polyimide, because their excellent mechanical properties. However, this class of materials contains a very large amount of carbon resulting in high absorption around the C K-edge.
Filters based on SiN are in general less transparent than most of used polymeric thin films like polyimide as it can be seen in Fig. 1 (calculated curves). To be competitive with polyimide the SiN membrane thickness shall be at least half the thickness of the polymer. In addition, the Si L edge at around 100 eV is quite pronounced significantly reducing the transmission up to the N K edge at around 400 eV.
Fig. 1
Comparison of the calculated transmission of 40 nm of polyimide (black dashed line), 40 nm of Si3N4 (green solid line), 30 nm of Si3N4 (light blue solid line), and 20 nm of Si3N4 (dark blue solid line).
On the other hand, being SiN carbon free, it may have niche applications when high transparency is required around the C K-edge region.
Performing a spectroscopic characterization of sandwiches composed of silicon nitride and aluminum is a fundamental step for designing filters with these materials; since their spectroscopic properties strongly depend both on their intrinsic properties and on their thickness and morphology.8
In this paper, we show a multi-technique investigation [UV-VIS-NIR spectroscopy, X-ray photoelectron spectroscopy (XPS), X-ray transmission spectroscopy, and atomic force microscopy (AFM)] of Al-coated ultra-thin silicon nitride membranes. Furthermore, a selection of these were irradiated with different proton doses, and then characterized by spectroscopy and AFM to assess any potential modifications in their properties. We measured the X-ray transmission of these materials and recovered the thicknesses of all the present layers by modeling. The analysis of X-ray photoelectron spectra allowed us to derive the thickness of the native aluminum oxide that reduces the nominal amount of metallic aluminum. We also studied these filter samples by UV/VIS/NIR spectroscopy to estimate the attenuation capability in this band, which is relevant in space when such filters are used to protect EUV/X-ray detectors from Sun light and out-of-band optical load from other astrophysical sources.
2.
Materials and Methods
2.1.
Samples
The membranes under investigation are made of silicon nitride, with aluminum coating applied on both surfaces. For reference a silicon nitride membrane without Al coating was also characterized. Some samples are supported by a mesh, consisting of a honeycomb structure with silicon bars thick and with a width of , and a pitch of , resulting in more than 80% open area (OA). When the mesh is present, it is placed between the one aluminum layer and the silicon nitride membrane. All the investigated samples were mounted on a small size metal frame, the standard TO-8 package used in semiconductor industries.9 The outer diameter of the cap is , the height and the clear aperture diameter hosting the thin membrane is 7 mm. An optical scan acquired using a photographic scanner EPSON Perfection V850 Pro in transmission and in reflection mode of a typical filter sample mounted on a TO-8 frame is reported in Fig. 2.
Fig. 2
Optical scan in transmission (a) and in reflection mode (b) of a typical sample mounted on a TO-8 standard frame with 7 mm clear aperture diameter.
The SiN layers were fabricated by low-pressure chemical vapor deposition, whereas the silicon mesh was patterned using standard lithography and plasma etching. The aluminum is deposited by sputtering deposition as reported in a previous paper.6 The main characteristics of the silicon nitride/aluminum membrane samples investigated in this paper are reported in Table 1. The aluminum amount is close to that corresponding to the baseline of the filters of both instruments of Athena.10 ,11 The samples with self-standing membranes (first four rows) were used to investigate the properties of pristine materials from a spectroscopic point of view, while the samples with membranes supported by a silicon mesh were mostly used to probe the radiation hardness.
Table 1
Main characteristics of the silicon nitride/aluminum membrane samples investigated in this paper. Sample name, nominal thicknesses of aluminum and silicon nitride, OA, and mesh features are reported.
Sample name | Al (nm) | SiN (nm) | OA (%) | Mesh features (μm) |
---|---|---|---|---|
TO8-C1-1 | 2 ×ばつ 10 ± 5% | 145 ± 5% | 100 | — |
TO8-C1-2 | 2 ×ばつ 10 ± 5% | 145 ± 5% | 100 | — |
TO8-C2-1#2 | 2 ×ばつ 10 ± 5% | 40 ± 5% | 100 | — |
TO8-C2-2#2 | 2 ×ばつ 10 ± 5% | 40 ± 5% | 100 | — |
TO8-C2-6 | 2 ×ばつ 15 ± 5% | 40 ± 5% | 82 | Bar height 15 |
Bar width 17 | ||||
Pitch size 200 | ||||
TO8-C2-1 | 2 ×ばつ 15 ± 5% | 40 ± 5% | 82 | Bar height 15 |
Bar width 17 | ||||
Pitch size 200 | ||||
TO8-C2-5a | 2 ×ばつ 15 ± 5% | 40 ± 5% | 82 | Bar height 15 |
Bar width 17 | ||||
Pitch size 200 | ||||
TO8-C2-2a | 2 ×ばつ 15 ± 5% | 40 ± 5% | 82 | Bar height 15 |
Bar width 17 | ||||
Pitch size 200 | ||||
TO8-C2-3a | 2 ×ばつ 15 ± 5% | 40 ± 5% | 82 | Bar height 15 |
Bar width 17 | ||||
Pitch size 200 | ||||
TO8-C2-31 | 0 | 40 ± 5% | 82 | Bar height 15 |
Bar width 17 | ||||
Pitch size 200 |
aSamples irradiated with 1 MeV protons.
2.2.
Proton Irradiation
1 MeV proton irradiation was performed at the Van der Graaf accelerator at the Johann Wolfgang Goethe-Universität Frankfurt am Main12 on a few samples supported by silicon mesh (Table 2). The irradiations were performed with different fluences, reported in Table 2, relative to the total non-ionizing radiation qualification fluence (Q.F.) equal to (equivalent to 10 MeV protons) corresponding to the radiation dose the Athena mission will undergo over the nominal lifetime of 4 years.
Table 2
List of samples supported by silicon mesh that have been irradiated with 1 MeV protons. The radiation dose is relative to Q.F.=1.2·1010 cm−2.
Sample name | Radiation dose (relative to Q.F.) |
---|---|
TO8-C2-5 | 1 |
TO8-C2-2 | 10 |
TO8-C2-3 | 100 |
2.3.
X-ray Photoelectron Spectroscopy
XPS measurements were performed on four filter samples TO8-C1-2, TO8-C2-2#2, TO8-C2-6, and TO8-C2-2. As aforementioned, the sample TO8-C2-2 was irradiated with a fluence equal to 10 Q.F. while the TO8-C2-6 was pristine.
XPS measurements were performed at the BACH beamline of the Elettra synchrotron (Trieste, Italy), which is equipped with a hemispherical electron analyzer (VG Scienta R3000) placed at 60° from the incident beam direction. The spot size of the beam was (horizontal ×ばつ vertical). The XPS spectra were recorded with linearly polarized synchrotron radiation, at a total instrumental resolution of 0.3 eV at 530 eV photon energy, and 0.5 eV at 1100 eV photon energy. We collected the Al 2p XPS spectra to estimate the amount of aluminum oxide, which is natively present on any aluminum surface. Binding energies of spectra were calibrated to Au (84.0 eV) measured on an Au foil in electric contact with the samples.
Fits have been carried out using the X-ray photoelectron spectroscopy tools program package,13 and a Shirley-type background, which is the typical function used to remove the background contribution caused by inelastic scattered electrons, was subtracted. Each peak is reproduced by a Gauss-Lorentzian sum function to approximate the Voigt profile. Al 2p XPS spectra were acquired in the experimental conditions reported in Table 3.
Table 3
Experimental conditions for the XPS data collection. The nominal kinetic energies of the outgoing electrons and the emission angle, α, with respect to surface normal are reported.
Sample name | KE of the photoemitted electron (eV) | α (deg) |
---|---|---|
TO8-C1-2 | 450, 550, and 750 | 0 |
TO8-C2-2#2 | 450, 550, and 750 | 0 |
TO8-C2-6 | 490, 800, and 1025 | 30 |
TO8-C2-2 | 450, 550, and 750 | 0 |
2.4.
X-ray Transmission Measurements
X-ray transmission measurements were carried out at two X-ray beamlines of the Physikalisch- Technische Bundesanstalt at the BESSY II synchrotron radiation facility in Berlin – Germany: in the photon energy range from 50 to 1800 eV at the PTB soft X-ray beamline14 and from 1750 to 3600 eV at the PTB Four-Crystal Monochromator (FCM) beamline.15 The energy range investigated includes edges of the elements present in the filter: Al L-edges @73 eV and @118 eV, Si L-edges @99 eV and @149 eV, N K-edge @402 eV, O K-edge @532 eV, Al K-edge @1560 eV and Si K-edge @1839 eV. The energy scans were done sequentially with the direct beam measured before and after the filter measurement to control for stability. Additionally, the signal measured with no beam on was subtracted from each measurement.
At the soft X-ray beamline, measurements were performed with a spectral resolving power better than 1000, the spot size was (vertical ×ばつ horizontal). Data near the C K-edge were not acquired since in this energy range the signal is insufficient due to carbon contamination of the beamline optics. The X-ray transmission measurements were performed at the soft X-ray beamline using different energy steps, as reported in Table 4.
Table 4
X-ray transmission measurements parameters adopted at PTB soft X-ray beamline.
Al L-edge | Si L-edge | N K-edge | O K-edge | Al K-edge | ||||||
---|---|---|---|---|---|---|---|---|---|---|
Energy range (eV) | 50 to 70 | 70 to 94 | 94 to 180 | 180 to 390 | 390 to 450 | 450 to 520 | 520 to 570 | 570 to 1550 | 1550 to 1700 | 1700 to 1800 |
Sample name | Energy step in each range (eV) | |||||||||
TO8-C1-1 | 2 | 0.2 | 0.2 | 5 | 0.4 | 5 | 0.4 | 20 | 1 | 10 |
TO8-C2-6 | 2 | 0.2 | 0.2 | 5 | 0.4 | 5 | 0.4 | 20 | 1 | 10 |
TO8-C2-5 | 2 | 0.2 | 0.2 | 5 | 0.4 | 5 | 0.4 | 20 | 1 | 10 |
TO8-C2-2 | 2 | 2 | 0.2 | 5 | 0.4 | 5 | 10 | 20 | 10 | 10 |
TO8-C2-31 | 2 | 2 | 0.2 | 5 | 0.4 | 5 | 10 | 20 | 10 | 10 |
The samples were also measured at PTB FCM15 beamline, where the measurements were performed with the InSb crystals in the monochromator, providing a spectral resolving power better than 4000. The spot size was . Transmission spectra are recorded in the energy range 1750 to 3600 eV, using different energy steps, as reported in Table 5.
Table 5
X-ray transmission measurement parameters adopted at the PTB FCM beamline.
Si K-edge | ||||
---|---|---|---|---|
Energy range (eV) | 1750 to 1830 | 1830 to 1900 | 1900 to 2200 | 2200 to 3600 |
Sample name | Energy step in each range (eV) | |||
TO8-C1-1 | 10 | 1 | 10 | 50 |
TO8-C2-6 | 10 | 1 | 10 | 50 |
TO8-C2-5 | 10 | 1 | 10 | 50 |
TO8-C2-2 | 10 | 1 | 10 | 50 |
TO8-C2-31 | 10 | 1 | 10 | 50 |
2.5.
UV/VIS/NIR Transmission
UV/VIS/NIR transmission spectra were collected at room temperature in transmission geometry using the double-beam spectrometer PerkinElmer Lambda1050+ available at the laboratory of INAF/OAPA. Given the small clear aperture diameter of the TO-8, a suitable sample holder was realized ad hoc to ensure high repeatability in positioning sample filters and an open TO-8 frame to acquire the blank spectra at the start of each measurement session. The measurement parameters were optimized by repeating transmission measurements for each filter to increase the signal-to-noise ratio. Data were collected in the 190 to 2000 nm range using a 2 nm data pitch.
2.6.
Atomic Force Microscopy
AFM measurements are acquired in air using a Bruker FAST-SCAN microscope. The images are obtained in tapping mode by using FAST-SCAN probes with an apical radius of about 5 nm. Each AFM image has a pixel resolution comparable to the tip size and surface micro-roughness resolution down to . The roughness of the surface has been measured over large areas of . Three different samples were measured; two of the measured samples are pristine, TO8-C2-1 and TO8-C2-6, and one has been irradiated with 100 times the QF, TO8-C2-3.
3.
Results and Discussion
All the Al 2p XPS spectra shown in Fig. 3 are composed of two main signals: a major contribution at higher binding energy attributed to the (oxidized aluminum) component and a minor signal at lower energy assigned to the component (metal aluminum). For the is possible to resolve the doublet due to the spin-orbit coupling which corresponds to the two possible states having distinguishable binding energies, attributed to and Al peaks.16
Fig. 3
Al 2p spectra of the TO8-C1-2 (first row), TO8-C2-2#2 (second row), TO8-C2-6 (third row), and TO8-C2-2 (fourth row) samples at different kinetic energies (KE) of the outgoing electrons. The specific KE is reported inside each plot.
Figure 3 shows that as the kinetic energy (KE) of the ejected electrons increases, the relative contribution of metallic aluminum increases with respect to the aluminum oxide. As the KE increases, the investigated thickness is larger, as the effective attenuation length (EAL) of the photoemitted electrons increases with the photon energy, thus more signal is detected from the deep metallic aluminum substrate with respect to the superficial oxide layer.
Assuming a flat homogeneous oxide layer on top of a homogenous Al substrate, the thickness of the aluminum oxide, , can be calculated using the following equation:17
Eq. (1)
Eq. (2)
The EALs are computed using the NIST EAL database18 and the TPP- 2M predictive formula.19 The values of the photoionization asymmetry parameter were taken from Ref. 20. The uncertainties of the EAL are considered for Al and 10.9 and 17.4 % is considered, respectively.18
For the overlayer, we assume the density of , band gap energy 7.0 eV21 and 24 valence electrons per molecule. The ratio between the atomic densities was set at 1.5 and the areas of the Al 2p components were obtained by fitting the Al 2p peaks. An example of peak analysis is reported in Fig. 4.
Fig. 4
XPS scan of the Al 2p peak at KE of 450 eV of the TO8-C1-2 sample. Data reported are experimental (black circles), best fit (red solid line), Al oxide 2p component (red filled curve) Al metal 2p1/2 (dark blue filled curve), and Al metal 2p3/2 (light blue filled curve).
The oxide thickness is calculated as the slope of the linear fit of Eq. (3), reported in Fig. 5
Eq. (3)
Fig. 5
Plot of versus the inverse of the logarithm of Eq. (1) (red circles) and linear fit (red line).
The oxide thicknesses computed for all analyzed spectra are reported in Table 6.
Table 6
Oxide thicknesses obtained from XPS analysis of the Al 2p peak for the TO8-C1-2, TO8-C2-2#2, TO8-C2-6, and TO8-C2-2 samples.
Sample name | Oxide thickness (nm) |
---|---|
TO8-C1-2 | 2.97 ± 0.19 |
TO8-C2-2#2 | 2.85 ± 0.18 |
TO8-C2-6 | 2.69 ± 0.17 |
TO8-C2-2 | 2.86 ± 0.18 |
Such values are in good agreement with the thickness of native oxide on bulk Al(111) and Al(100) crystals16 and with the oxide thickness that was found in witness samples of the current baseline filters for the Athena X-ray integral field unit and WFI detectors,22 while it is very different to the case of the XMM back-up filters monitored over time.23 In the last case, the aluminum oxide thickness was found to be 5.9 nm, thus nearly twice that measured for the samples investigated in this paper.
The main purpose of the X-ray transmission measurements performed at BESSY II was to model the transmission curve of each filter, derive the areal density of the filter material and the thickness of each layer, with its associated uncertainties. Two fit functions were used, one involving the single atoms (elements) and disregarding the stoichiometry,24 and the other using the chemical formula of each layer of the filter material.
The fit using elements has up to four parameters, namely each atomic areal density
Eq. (4)
The fit function is based on the product of the transmission due to the i-th element , and has four free parameters, the areal density of each element. The quantity is the mass attenuation coefficient of the ’th chemical element and is calculated from the atomic scattering factors by Henke et al.25 Hydrogen was not included since it does not contribute to the transmission of the filter in the investigated energy range. In principle, all layer thicknesses can be estimated, introducing two quantities a posteriori: material density and stoichiometry [see Eqs. (5) and (6)]. From one can approximately calculate the thickness of the Al layer by dividing it for the Al bulk density of (in so doing, one considers only the aluminum in bulk form). To estimate the silicon nitride thickness, one can calculate the equivalent thickness, within the using a stoichiometry
Eq. (5)
Eq. (6)
The fit using materials has up to three parameters, namely each material thickness
Eq. (7)
The second material is a layer of aluminum oxide, whose presence is a well-established fact in the literature and is proven by the XPS measurements reported above. The advantage of using materials instead of atoms lies in that it is possible to directly obtain each layer thickness (using the following densities: , , and ) and make a comparison with the nominal thicknesses. A correction needs to be introduced for the filters supported by a mesh, to consider the OA and the mesh material, which is not generally opaque and could be transparent to X-rays at the higher end of the investigated energy spectrum. To this end, two more parameters were considered, namely the mesh material areal density and the OA, as seen by the beam spot (which is generally different from the nominal value)
Eq. (8)
Two best fits, one using elements and one using materials, were obtained for all the filter samples. For filters with a mesh, the additional parameters of mesh areal density and OA were derived. The areal densities and OA of the best fit on elements and the derived thicknesses are summarized in Table 7, whilst the layer thicknesses, mesh thickness and OA obtained from the best fit on materials are reported in Table 8.
Table 7
Areal densities of each element (Al, Si, O, N, and Si mesh) and OA with 3σ statistical uncertainty.
Sample name | Areal densities (10−7 g/cm2) | Si mesh thickness (μm) | OA (%) | Al equivalent thickness (nm) | SiN equivalent thickness (nm) | |||
---|---|---|---|---|---|---|---|---|
Al | Si | O | N | |||||
TO8-C1-1 | 54 ± 2 | 280 ± 3 | 0 ± 3 | 205 ± 3 | — | — | 20 ± 1 | 149 ± 2 |
TO8-C2-6 | 94 ± 2 | 75 ± 2 | 18 ± 2 | 67 ± 2 | 34 ± 2 | 84 ± 1 | 35 ± 1 | 48 ± 2 |
TO8-C2-5 | 89 ± 1 | 74 ± 1 | 8 ± 1 | 60 ± 1 | 32 ± 1 | 84 ± 1 | 33 ± 1 | 44 ± 2 |
TO8-C2-2 | 92 ± 2 | 70 ± 2 | 22 ± 2 | 59 ± 2 | 32 ± 2 | 83 ± 1 | 34 ± 1 | 43 ± 2 |
TO8-C2-31 | — | 79 ± 1 | 0 ± 1 | 56 ± 2 | 32 ± 2 | 82 ± 1 | — | 41 ± 2 |
The measured X-ray transmission spectra of the investigated filters are shown in Figs. 6 Fig. 7 Fig. 8 Fig. 9–10 along with the best fits and details at the absorption edges of the involved elements. In general, all fits are globally good, also at the Al, Si, and N edges, but discrepancies are visible at the O edges, partly related to the low amount of O.
Fig. 6
Experimental data (black points) of TO8-C1-1 filter and the best fit on elements (red line).
Fig. 7
Experimental data (black points) of TO8-C2-6 filter and the best fit on elements (red line).
Fig. 8
Experimental data (black points) of TO8-C2-5 filter and the best fit on elements (red line).
Fig. 9
Experimental data (black points) of TO8-C2-2 filter and the best fit on elements (red line).
Fig. 10
Experimental data (black points) of TO8-C2-31 filter and the best fit on elements (red line).
As can be seen in Table 8, the sum of the Al and the thicknesses is in agreement, within the uncertainties, with the equivalent thicknesses of the Al layer, calculated from the areal densities in Table 7. In most cases, it is slightly higher than the nominal Al thickness. Furthermore, for the samples with the thin silicon nitride substrate, the thickness varies from sample to sample, probably due to the fit being less accurate around the O K-edge. The obtained thickness of the SiN substrate itself deviates only a few percent from the nominal values. The obtained OA from both fits is also close to the nominal value. Estimating the mesh thickness is trickier, because both the OA and the mesh areal density are interdependent parameters and difficult to disentangle for the optimization algorithm.
Table 8
Layer thickness of each material (Al, Al2O3, SiN, SiO2, and Si mesh) and OA with 3σ statistical uncertainty and nominal thickness for all filters.
Best fit thicknesses | Nominal thicknesses | (%) | |||||||
---|---|---|---|---|---|---|---|---|---|
Sample name | Al (nm) | SiN (nm) | Al2O3 (nm) | Si mesh (μm) | OA (%) | Al (nm) | SiN (nm) | Si mesh (μm) | OA |
TO8-C1-1 | 18 ± 2 | 142 ± 1 | 3.0 ± 1 | — | — | 2 ×ばつ 10 | 145 | — | — |
TO8-C2-6 | 22 ± 1 | 41 ± 1 | 17 ± 1 | 15 ± 1 | 84 ± 1 | 2 ×ばつ 15 | 40 | 15 | 82 |
TO8-C2-5 | 26 ± 1 | 39 ± 1 | 8 ± 1 | 14± | 83 ± 1 | 2 ×ばつ 15 | 40 | 15 | 82 |
TO8-C2-2 | 21 ± 1 | 37 ± 1 | 18 ± 1 | 13 ± 1 | 83 ± 1 | 2 ×ばつ 15 | 40 | 15 | 82 |
TO8-C2-31 | — | 39 ± 1 | — | 13 ± 1 | 82 ± 1 | — | 40 | 15 | 81 |
Transmission spectra acquired in the UV/VIS/NIR range are reported in Figs. 11 and 12. The reported spectra show that these filters are quite transparent in the UV region (190 to 400 nm), partly due to the constructive interference effects generated by the bilayer of aluminum, while in the visible portion of the spectra the rejection of the radiation is more efficient.
The shape of the transmission curves of Fig. 12 does not look affected by the irradiation treatment, suggesting that these multilayers are quite resistant when proton irradiation occurs. Although a blueshift of the main peak (close to 300 nm) must be noticed when the Q.F. increases, this peak moves from 312 nm (pristine filter, 3.97 eV) to 302 nm (1 Q.F. sample, 4.11 eV) and to 296 nm (10 Q.F., 4.19 eV).
Fig. 11
UV/VIS/NIR transmission of meshless samples the TO8-C1-1 (black line) and TO8-C2-1#2 (red line).
Fig. 12
UV/VIS/NIR transmission of samples with meshes with different proton irradiation doses, namely: the TO8-C2-6 (0 Q.F. black line), the TO8-C2-5 (1 Q.F. blue line), and TO8-C2-2 (10 Q.F. red line).
Zhang et al. showed that the position of the aluminum absorption band close to 4 eV is size-dependent: if the size of the nanoparticle increases, the peak redshifts.26 Then the observed blueshift in our work might be ascribed to a slight reduction of the size of aluminum nanoparticles assembled to create the metal coating.
AFM images were analyzed using the data analysis software Gwyddion27 and are reported in Fig. 13. The zero-height reference is located in the lowest point measured by the probe.
Fig. 13
AFM data and analysis. (a)–(b) The 3D images of the upper images of the TO8-C2-1, TO8-C2-6, and TO8-C2-3, respectively. (d)–(f) Typical height profiles of the TO8-C2-1, TO8-C2-6, and TO8-C2-3, respectively. (g)–(i) The histograms of the above height profiles (red columns) and the fit (black line) of the TO8-C2-1, TO8-C2-6, and TO8-C2-3, respectively.
Since in literature it is found that ion irradiation can affect the aluminum surface28 ,29 and that proton irradiation may create ripples and hillocks changing the roughness of the surfaces,30 both the roughness and the average heights are computed.
The roughness, , of the samples was calculated as reported in the following equation:
Eq. (9)
The height data, obtained from the z-profiles [Figs. 13(d)–13(f)], are reported in three histogram plots [Figs. 13(g)–13(i)], and fitted using a Gaussian curve. The average heights correspond to the maxima of the fits. The obtained average heights for the samples TO8-C2-1, TO8-C2-6, and TO8-C2-3 are 12.75 nm, 13.78 nm, and 9.32 nm, respectively. The AFM analysis suggests that the average heights of the pristine samples are larger than the irradiated filter, this may hint at the possibility of an erosion process due to the proton exposure as suggested by Sznajder et al.31
4.
Conclusions
The analyses of the XPS spectra we reported show that Al/SiN/Al is undoubtedly oxidized on the surface. The thickness values that we find for the surface oxide agree with other results, already reported in the literature, for Al-coated polymeric filters.20 ,21 The irradiation treatment has no relevant effect on the surface oxide thickness up to 10 Q.F. On the other hand, the amount of oxide revealed by the X-ray transmission measurement is larger than the one obtained by XPS, because this technique is sensitive to the bulk, consequently, the whole amount of the present aluminum oxide is detected: both the two layers on the two external coating surfaces and any interfacial Al oxide between the silicon nitride and the aluminum coating. Moreover, the amount of Al oxide computed by the X-ray transmission model might be affected by the presence of , which can be found on the silicon mesh and/or the silicon nitride.
Both surface roughness and UV/VIS/NIR transmission are not significantly affected by proton irradiation. The samples we studied are rather transparent below 400 nm; this can be ascribed to a total small amount of aluminum (20 nm) of which at least 20% is oxidized. To design an effective OBF for use in high energy astrophysical space missions based on SiN, the amount of Al must be increased to at least 30 nm possibly deposited on a single side to reduce the aluminum oxidation. However, this choice would cause a low transmission in the soft X-rays, that for the investigated samples is already at 0.5 keV. These materials can be proposed in those cases where the presence of carbon atoms might be an issue although the capability to manufacture very thin large area membranes and their mechanical performances under differential pressure and dynamic launch stresses needs to be demonstrated.