Ex-situ spectroscopic ellipsometry measurements are made on radio frequency magnetron sputtered oxygenated cadmium sulfide (CdS:O) thin films. Films are deposited onto glass substrates at room temperature and at 270 °C with varying oxygen to total gas flow ratios in the sputtering ambient. Ellipsometric spectra from 0.74 to 5.89 eV are collected before and after annealing at 607 °C to simulate the thermal processes during close-space sublimation of overlying cadmium telluride in that solar cell configuration. Complex dielectric function (ε = ε1 + iε2) spectra are extracted for films as a function of oxygen gas flow ratio, deposition temperature, and post-deposition annealing using a parametric model accounting for critical point transitions and an Urbach tail for sub-band gap absorption. The results suggest an inverse relationship between degree of crystallinity and oxygen gas flow ratio, whereas annealing is shown to increase crystallinity in all samples. Direct band gap energies are determined from the parametric modeling of ε and linear extrapolations of the square of the absorption coefficient. As-deposited samples feature a range of band gap energies whereas annealing is shown to result in gap energies ranging only from 2.40 to 2.45 eV, which is close to typical band gaps for pure cadmium sulfide.
INTRODUCTION
Cadmium sulfide (CdS) thin films are commonly used as n-type window layers in various thin film solar cell configurations, most notably cadmium telluride (CdTe)1,2 and copper indium gallium selenide1,3 photovoltaic (PV) devices. As has been detailed elsewhere4 for the case of CdTe cells, overall device performance can be restricted by CdS layers because of a tradeoff between greater short-wavelength absorption in thicker CdS layers and poorer open circuit voltage and fill factor in devices fabricated with thinner CdS layers. One strategy for overcoming such limitations has been to increase the band gap of CdS by incorporating oxygen, thereby allowing optimal thicknesses with a greater amount of the incident solar spectrum reaching the underlying PV absorber. CdTe devices made with oxygenated CdS (CdS:O) window layers have shown promising results,5,6 with a maximum conversion efficiency of 15.5% reported.4 While these studies have confirmed that the use of CdS:O window layers can potentially improve the performance of CdTe solar cells, further investigation on the effects of close-space sublimation (CSS) of CdTe on the properties of underlying CdS:O as is found in the CdTe solar cell configuration is needed. This CSS of CdTe is typically done at temperatures above 500 °C, which is more than sufficient to alter the initial structure and optical properties of CdS:O deposited at lower temperatures. It has been reported by Paudel et al.6 that by exposing as-deposited CdS:O layers to the temperature, pressure, and ambient gas composition encountered during the CSS processing, crystallinity in the films increases and the band gap energies revert to values similar to that of CdS. In that study, however, band gap determinations were performed using unpolarized transmittance spectroscopy of relatively thick films (3000–4000 Å) with incident wavelengths limited to the 300–1000 nm range (4.13–1.24 eV). Those films are not completely representative of the <1000 Å thick CdS or CdS:O layers typically used in high performance CdTe solar cells. Additionally, the material-specific optical properties obtained using those measurements are mainly limited to the absorption coefficient (α), and from this the band gap energy (Eg), which provides only a cursory understanding of the optical response of these films both before and after high temperature processing.
Optimization of CdS:O films for opto-electronic devices like thin film solar cells requires a detailed understanding of their optical response. Previous studies of CdS:O films have demonstrated the effectiveness of applying spectroscopic ellipsometry in determining the influence of some fabrication and processing conditions on resultant optical properties.7–9 These studies, however, have not examined important intermediate oxygen gas flow ratios and high temperature processing consistent with full CdTe device fabrication, and they do not exhibit sufficient sensitivity to accurately model higher energy, above band gap critical point transitions in CdS and CdS:O. This work represents a comprehensive study of the effects of deposition temperature and subsequent processing conditions similar to CSS of CdTe on CdS:O films for use in CdTe solar cells, as evaluated using a physically realistic optical property model developed to retain sensitivity to critical point transitions in disordered, but polycrystalline, CdS:O films.
EXPERIMENTAL DETAILS
Two series of CdS:O films have been deposited onto soda lime glass substrates. The glass has been prepared using a detergent-based (Micro-90, International Products Corp.) cleaning procedure assisted by ultrasonication to ensure chemically clean surfaces. Radio frequency (RF) magnetron reactive sputtering (frequency = 13.56 MHz) has been used to deposit the CdS:O in 10 mTorr ambient with the proportion of O2 gas adjusted by controlling the flow rates of separate streams of pure Ar and 5% volume fraction O2 in Ar, with the total combined flow rate maintained at 40 sccm. Each series consists of films grown with O2 gas flow ratios 100% × [O2]/{[Ar] + [O2]} = 0% (CdS), 1%, 2%, and 3% volume fractions, with one series deposited with no intentional substrate heating (i.e., at room temperature denoted RT) and the other with the substrate heated to 270 °C. Each sample is annealed at a temperature of 607 °C in 99.5% He + 0.5% O2 volume fractions at 50 Torr to simulate the CSS CdTe processing conditions that would follow CdS:O deposition in the PV device fabrication sequence. Further details about the fabrication and processing of these samples are described elsewhere.6
Ellipsometric spectra (in N = cos 2Ψ, C = sin 2Ψ cos Δ, and S = sin 2Ψ sin Δ) for all the samples have been measured at RT over a spectral range of 0.74 to 5.89 eV using a single rotating compensator multichannel ellipsometer10,11 (Model M-2000FI, J. A. Woollam Co., Inc.) both before and after annealing at 607 °C. A stratified structural model has been developed to extract layer thicknesses and optical properties in the form of complex dielectric function (ε = ε1 + iε2) spectra. The parameters describing the model are iteratively fit using a least-squares regression that minimized the unweighted error function12 between the model simulation and measured ellipsometric spectra as shown in Figure 1. The structural model consists of a semi-infinite glass substrate, bulk CdS:O layer of thickness db, and surface roughness of thickness ds as shown schematically in Figure 1. The optical properties of the roughness layer are described by a Bruggeman effective medium approximation13,14 consisting of fv volume fraction void and 1−fv fraction material identical to the underlying CdS:O. Spectra in ε describing the substrate are described by a Sellmeier oscillator and a constant additive term to ε1, ε∞, when fitting to ellipsometric measurements collected for a bare piece of identical soda lime glass.15,16 The optical properties of the CdS:O are represented by a hybrid parameterization of ε. Spectra in ε2 are described by the sum of oscillators assuming critical point parabolic band (CPPB) transitions17 above the lowest energy critical point (E0) (i.e., photon energies where the films are strongly absorbing) and an Urbach tail15 below E0. Then, spectra in ε1 are calculated as the sum of a high-energy Sellmeier oscillator, a constant ε∞ term, and Kramers–Kronig integration15 of corresponding spectra in ε2 to ensure that ε remains physically realistic. Thus, the full parameterization of ε used for the CdS:O materials can be written
where Aj, θj, Γj, and Ej are the CPPB amplitude, phase projection factor, broadening, and resonance energy of the jth interband transition, respectively; μj is fixed at 0.5 for one dimensional critical points; Eu is the Urbach energy; As and Es are the Sellmeier amplitudes and resonance energies, respectively; and P is the principal value of the Kramers–Kronig integral. It should be noted that x-ray diffraction measurements of similar but thicker CdS:O films6 and atomic force microscopy measurements of both these films and the corresponding thicker films confirmed the predominantly polycrystalline CdS:O structure, thereby validating the use of CPPB oscillators to describe ε for photon energies where the films are absorbing. As will be discussed in greater detail later, the sharpness and distinguishability of individual features in ε vary significantly with sample processing conditions, in particular, ambient O2 gas flow ratio during sputtering. Comparison of spectra in ε for each sample indicates that the film prepared at 0% oxygen flow ratio, 270 °C deposition temperature, and (post-deposition) annealed (0%/270 °C/annealed) most closely resembles ε of highly crystalline CdS films as has been reported elsewhere.18 Therefore, the phase projection factors θj of the three critical points within the measurement range (hereafter referred to as E0, E1–A, and E1–B) are fixed for all samples to the values determined for the 0%/270 °C/annealed sample. This decrease in the number of fitting parameters is essential for reliably extracting ε of the other samples, especially those with broader, less distinct features in ε.
Example model fit (black line) to measured ellipsometric spectra in N = cos 2Ψ, C = sin 2Ψ cos Δ, and S = sin 2Ψ sin Δ (colored circles) for as-deposited CdS:O film prepared at 0% oxygen gas flow ratio and 270 °C substrate temperature. Structural model schematic used to generate the model simulation is shown in the inset.
Example model fit (black line) to measured ellipsometric spectra in N = cos 2Ψ, C = sin 2Ψ cos Δ, and S = sin 2Ψ sin Δ (colored circles) for as-deposited CdS:O film prepared at 0% oxygen gas flow ratio and 270 °C substrate temperature. Structural model schematic used to generate the model simulation is shown in the inset.
RESULTS AND DISCUSSION
Spectra in ε for each sample are plotted in Figure 2, and the corresponding model parameter values and overall spectrally averaged mean square error (MSE) are reported in Table I. In addition to the E0 transition, we have independently resolved the E1–A and E1–B critical points and modeled their dependence on CdS:O film processing. These closely spaced features are easily distinguished for samples prepared at low oxygen gas flow ratios, but films prepared with increasing oxygen flow ratios generally have increasingly broad absorption features, sometimes making the E1–A and E1–B critical points difficult to individually resolve. In the most extreme cases, the indistinguishability of these critical points led to unacceptably high error associated with many of the E1–A and E1–B parameters, necessitating the use of a single CPPB oscillator to model the higher energy features in ε, as is seen for the 3%/270 °C/annealed, 3%/270 °C/as-deposited, 2%/RT/as-deposited, and 3%/RT/as-deposited samples. Additionally, ds could not be determined with acceptable error for three of those samples and is therefore fixed to 0 Å. The location and values of the E1–A and E1–B peaks in ε2 for the 0%/270 °C/annealed sample are in good agreement with the published literature.18–20 Such agreement with other studies further justifies the identification of that sample as the “best crystalline quality” CdS sample and its suitability for determining the θj phase projection factors.
Complex dielectric function (ε = ε1 + iε2) spectra for CdS:O films prepared as functions of oxygen gas flow ratio during sputtering (0%–3%), deposition temperature (270 °C or room temperature denoted RT), and both before and after post-deposition annealing at 607 °C.
Complex dielectric function (ε = ε1 + iε2) spectra for CdS:O films prepared as functions of oxygen gas flow ratio during sputtering (0%–3%), deposition temperature (270 °C or room temperature denoted RT), and both before and after post-deposition annealing at 607 °C.
Parameters describing spectra in ε as well as structural parameters including surface roughness thickness (ds), void fraction percentage in the surface roughness layer (fv), and bulk film thickness (db) for CdS:O films prepared as functions of oxygen gas flow ratio during sputtering (0%–3%), deposition temperature (270 °C or room temperature denoted RT), and both before and after post-deposition annealing at 607 °C.
. | 270 °C annealed . | 270 °C as-deposited . | ||||||
---|---|---|---|---|---|---|---|---|
O2 Gas flow ratio (%) . | 0 . | 1 . | 2 . | 3 . | 0 . | 1 . | 2 . | 3 . |
MSE (×10−3) | 3.196 | 2.154 | 1.976 | 2.463 | 1.781 | 2.018 | 1.951 | 2.785 |
db (Å) | 850 ± 2 | 810 ± 2 | 591.3 ± 0.8 | 80 ± 50 | 918 ± 2 | 864 ± 2 | 606 ± 2 | 171 ± 3 |
ds (Å) | 166 ± 2 | 112 ± 1 | 146.9 ± 0.6 | 220 ± 50 | 109 ± 2 | 96 ± 2 | 133 ± 2 | 0 (fixed) |
fv (%) | 22.0 ± 0.2 | 33.1 ± 0.5 | 65.0 ± 0.5 | 48 ± 7 | 14.5 ± 0.3 | 30.0 ± 0.6 | 26.5 ± 0.4 | … |
ε∞ | 1.93 ± 0.04 | 1.62 ± 0.04 | 1.63 ± 0.04 | 1.2 ± 0.1 | 1.45 ± 0.03 | 1.45 ± 0.05 | 1.53 ± 0.04 | 1.70 ± 0.04 |
Es (eV) | 6.79 ± 0.04 | 7.05 ± 0.04 | 7.12 ± 0.04 | 7.5 ± 0.2 | 7.09 ± 0.03 | 7.21 ± 0.05 | 7.08 ± 0.04 | 6.98 ± 0.04 |
As (eV2) | 11.8 ± 0.5 | 15.8 ± 0.5 | 16.2 ± 0.6 | 25 ± 8 | 17.8 ± 0.5 | 18.4 ± 0.7 | 16.0 ± 0.5 | 11.5 ± 0.4 |
Eu (eV) | 0.048 ± 0.001 | 0.062 ± 0.004 | 0.099 ± 0.003 | 0.134 ± 0.008 | 0.1062 ± 0.0009 | 0.078 ± 0.004 | 0.069 ± 0.004 | 0.54 ± 0.04 |
E0 (eV) | 2.452 ± 0.005 | 2.412 ± 0.009 | 2.41 ± 0.02 | 2.40 ± 0.03 | 2.445 ± 0.002 | 2.21± 0.01 | 2.14 ± 0.02 | 2.537 ± 0.008 |
A0 (eV−0.5) | 6.1 ± 0.5 | 5.7 ± 0.3 | 4.1 ± 0.4 | 0.9 ± 0.4 | 3.4 ± 0.1 | 4.6 ± 0.3 | 4.5 ± 0.3 | 2.67 ± 0.06 |
Γ0 (eV) | 0.110 ± 0.006 | 0.221 ± 0.009 | 0.19 ± 0.02 | 0.36 ± 0.03 | 0.155 ± 0.003 | 0.30 ± 0.01 | 0.43 ± 0.02 | 1.41 ± 0.05 |
E1-A (eV) | 4.777 ± 0.008 | 4.795 ± 0.007 | 5.038 ± 0.009 | 5.42 ± 0.03 | 4.893 ± 0.005 | 4.79 ± 0.02 | 4.65 ± 0.02 | 4.92 ± 0.03 |
A1-A (eV−0.5) | 12.0 ± 0.2 | 8.7 ± 0.3 | 7.6 ± 0.1 | 3 ± 1 | 9.9 ± 0.2 | 7.9 ± 0.4 | 4.9 ± 0.3 | 4.22 ± 0.07 |
Γ1-A (eV) | 0.77 ± 0.02 | 0.38 ± 0.03 | 1.06 ± 0.01 | 2.0 ± 0.1 | 1.03 ± 0.01 | 0.76 ± 0.03 | 0.71 ± 0.04 | 1.96 ± 0.06 |
E1-B (eV) | 5.37 ± 0.02 | 5.20 ± 0.01 | 5.444 ± 0.007 | 4.90 ± 0.01 | 5.29 ± 0.02 | 5.15 ± 0.02 | ||
A1-B (eV−0.5) | 4.3 ± 0.4 | 6.7 ± 0.3 | 3.5 ± 0.3 | 2.7 ± 0.3 | 5.1 ± 0.4 | 5.7 ± 0.4 | ||
Γ1-B (eV) | 0.18 ± 0.04 | 0.88 ± 0.02 | 0.16 ± 0.03 | 0.18 ± 0.04 | 0.72 ± 0.05 | 1.09 ± 0.02 | ||
θ0 (°) | −74 ± 2 | |||||||
θ1-A (°) | 23 ± 1 | |||||||
θ1-B (°) | 26 ± 7 |
. | 270 °C annealed . | 270 °C as-deposited . | ||||||
---|---|---|---|---|---|---|---|---|
O2 Gas flow ratio (%) . | 0 . | 1 . | 2 . | 3 . | 0 . | 1 . | 2 . | 3 . |
MSE (×10−3) | 3.196 | 2.154 | 1.976 | 2.463 | 1.781 | 2.018 | 1.951 | 2.785 |
db (Å) | 850 ± 2 | 810 ± 2 | 591.3 ± 0.8 | 80 ± 50 | 918 ± 2 | 864 ± 2 | 606 ± 2 | 171 ± 3 |
ds (Å) | 166 ± 2 | 112 ± 1 | 146.9 ± 0.6 | 220 ± 50 | 109 ± 2 | 96 ± 2 | 133 ± 2 | 0 (fixed) |
fv (%) | 22.0 ± 0.2 | 33.1 ± 0.5 | 65.0 ± 0.5 | 48 ± 7 | 14.5 ± 0.3 | 30.0 ± 0.6 | 26.5 ± 0.4 | … |
ε∞ | 1.93 ± 0.04 | 1.62 ± 0.04 | 1.63 ± 0.04 | 1.2 ± 0.1 | 1.45 ± 0.03 | 1.45 ± 0.05 | 1.53 ± 0.04 | 1.70 ± 0.04 |
Es (eV) | 6.79 ± 0.04 | 7.05 ± 0.04 | 7.12 ± 0.04 | 7.5 ± 0.2 | 7.09 ± 0.03 | 7.21 ± 0.05 | 7.08 ± 0.04 | 6.98 ± 0.04 |
As (eV2) | 11.8 ± 0.5 | 15.8 ± 0.5 | 16.2 ± 0.6 | 25 ± 8 | 17.8 ± 0.5 | 18.4 ± 0.7 | 16.0 ± 0.5 | 11.5 ± 0.4 |
Eu (eV) | 0.048 ± 0.001 | 0.062 ± 0.004 | 0.099 ± 0.003 | 0.134 ± 0.008 | 0.1062 ± 0.0009 | 0.078 ± 0.004 | 0.069 ± 0.004 | 0.54 ± 0.04 |
E0 (eV) | 2.452 ± 0.005 | 2.412 ± 0.009 | 2.41 ± 0.02 | 2.40 ± 0.03 | 2.445 ± 0.002 | 2.21± 0.01 | 2.14 ± 0.02 | 2.537 ± 0.008 |
A0 (eV−0.5) | 6.1 ± 0.5 | 5.7 ± 0.3 | 4.1 ± 0.4 | 0.9 ± 0.4 | 3.4 ± 0.1 | 4.6 ± 0.3 | 4.5 ± 0.3 | 2.67 ± 0.06 |
Γ0 (eV) | 0.110 ± 0.006 | 0.221 ± 0.009 | 0.19 ± 0.02 | 0.36 ± 0.03 | 0.155 ± 0.003 | 0.30 ± 0.01 | 0.43 ± 0.02 | 1.41 ± 0.05 |
E1-A (eV) | 4.777 ± 0.008 | 4.795 ± 0.007 | 5.038 ± 0.009 | 5.42 ± 0.03 | 4.893 ± 0.005 | 4.79 ± 0.02 | 4.65 ± 0.02 | 4.92 ± 0.03 |
A1-A (eV−0.5) | 12.0 ± 0.2 | 8.7 ± 0.3 | 7.6 ± 0.1 | 3 ± 1 | 9.9 ± 0.2 | 7.9 ± 0.4 | 4.9 ± 0.3 | 4.22 ± 0.07 |
Γ1-A (eV) | 0.77 ± 0.02 | 0.38 ± 0.03 | 1.06 ± 0.01 | 2.0 ± 0.1 | 1.03 ± 0.01 | 0.76 ± 0.03 | 0.71 ± 0.04 | 1.96 ± 0.06 |
E1-B (eV) | 5.37 ± 0.02 | 5.20 ± 0.01 | 5.444 ± 0.007 | 4.90 ± 0.01 | 5.29 ± 0.02 | 5.15 ± 0.02 | ||
A1-B (eV−0.5) | 4.3 ± 0.4 | 6.7 ± 0.3 | 3.5 ± 0.3 | 2.7 ± 0.3 | 5.1 ± 0.4 | 5.7 ± 0.4 | ||
Γ1-B (eV) | 0.18 ± 0.04 | 0.88 ± 0.02 | 0.16 ± 0.03 | 0.18 ± 0.04 | 0.72 ± 0.05 | 1.09 ± 0.02 | ||
θ0 (°) | −74 ± 2 | |||||||
θ1-A (°) | 23 ± 1 | |||||||
θ1-B (°) | 26 ± 7 |
. | RT annealed . | RT as-deposited . | ||||||
---|---|---|---|---|---|---|---|---|
O2 Gas flow ratio (%) . | 0 . | 1 . | 2 . | 3 . | 0 . | 1 . | 2 . | 3 . |
MSE (×10−3) | 2.899 | 3.431 | 4.030 | 5.171 | 2.439 | 2.815 | 6.339 | 7.702 |
db (Å) | 589 ± 1 | 550.50 ± 0.08 | 454 ± 1 | 390 ± 10 | 707.8 ± 0.5 | 641 ± 3 | 606.8 ± 0.8 | 578 ± 1 |
ds (Å) | 108 ± 2 | 168 ± 5 | 368 ± 8 | 550 ± 20 | 201 ± 7 | 85 ± 1 | 0 (fixed) | 0 (fixed) |
fv (%) | 72 ± 1 | 83.0 ± 0.6 | 93.1 ± 0.2 | 92.8 ± 0.5 | 90.2 ± 0.4 | 51 ± 2 | … | … |
ε∞ | 1.23 ± 0.08 | 1.3 ± 0.1 | 1.5 ± 0.2 | 2.9 ± 0.1 | 1.99 ± 0.05 | 1.49 ± 0.06 | 2.02 ± 0.06 | 2.03 ± 0.07 |
Es (eV) | 7.35 ± 0.07 | 7.7 ± 0.1 | 8.1 ± 0.2 | 6.4 ± 0.1 | 7.22 ± 0.05 | 7.16 ± 0.05 | 6.69 ± 0.06 | 6.72 ± 0.07 |
As (eV2) | 23 ± 1 | 22 ± 2 | 23 ± 3 | 1.5 ± 0.5 | 17.0 ± 0.7 | 20.8 ± 0.9 | 10.5 ± 0.7 | 10.30 ± 0.08 |
Eu (eV) | 0.054 ± 0.006 | 0.054 ± 0.006 | 0.080 ± 0.007 | 0.038 ± 0.006 | 0.100 ± 0.007 | 0.04 ± 0.01 | 0.06 ± 0.02 | 0.11 ± 0.03 |
E0 (eV) | 2.430 ± 0.007 | 2.43 ± 0.02 | 2.41 ± 0.04 | 2.423 ± 0.008 | 2.39 ± 0.02 | 2.30 ± 0.06 | 2.71 ± 0.09 | 3.1 ± 0.2 |
A0 (eV−0.5) | 7.4 ± 0.4 | 5.2 ± 0.7 | 3.7 ± 0.8 | 2.6 ± 0.3 | 3.8 ± 0.3 | 3.0 ± 0.2 | 4.1 ± 0.5 | 3.9 ± 0.8 |
Γ0 (eV) | 0.13 ± 0.01 | 0.19 ± 0.02 | 0.26 ± 0.03 | 0.29 ± 0.02 | 0.37 ± 0.03 | 1.04 ± 0.08 | 1.1 ± 0.1 | 1.2 ± 0.3 |
E1-A (eV) | 5.07 ± 0.02 | 4.98 ± 0.02 | 4.92 ± 0.06 | 4.72 ± 0.06 | 4.97 ± 0.01 | 5.19 ± 0.02 | 5.12 ± 0.02 | 5.29 ± 0.06 |
A1-A (eV−0.5) | 8.6 ± 0.3 | 7.0 ± 0.2 | 6.1 ± 0.7 | 4.6 ± 0.3 | 2.0 ± 0.2 | 5.9 ± 0.2 | 5.0 ± 0.1 | 3.6 ± 0.2 |
Γ1-A (eV) | 0.98 ± 0.01 | 1.05 ± 0.02 | 1.03 ± 0.07 | 1.0 ± 0.1 | 0.23 ± 0.06 | 1.26 ± 0.02 | 1.99 ± 0.06 | 2.7 ± 0.3 |
E1-B (eV) | 5.45 ± 0.01 | 5.44 ± 0.01 | 5.39 ± 0.05 | 5.4 ± 0.1 | 5.30 ± 0.01 | 5.72 ± 0.02 | ||
A1-B (eV−0.5) | 4.6 ± 0.4 | 2.7 ± 0.3 | 2.1 ± 0.9 | 1.1 ± 0.4 | 5.8 ± 0.2 | 2.6 ± 0.3 | ||
Γ1-B (eV) | 0.22 ± 0.05 | 0.25 ± 0.07 | 0.5 ± 0.2 | 0.7 ± 0.3 | 1.22 ± 0.03 | 0.28 ± 0.08 |
. | RT annealed . | RT as-deposited . | ||||||
---|---|---|---|---|---|---|---|---|
O2 Gas flow ratio (%) . | 0 . | 1 . | 2 . | 3 . | 0 . | 1 . | 2 . | 3 . |
MSE (×10−3) | 2.899 | 3.431 | 4.030 | 5.171 | 2.439 | 2.815 | 6.339 | 7.702 |
db (Å) | 589 ± 1 | 550.50 ± 0.08 | 454 ± 1 | 390 ± 10 | 707.8 ± 0.5 | 641 ± 3 | 606.8 ± 0.8 | 578 ± 1 |
ds (Å) | 108 ± 2 | 168 ± 5 | 368 ± 8 | 550 ± 20 | 201 ± 7 | 85 ± 1 | 0 (fixed) | 0 (fixed) |
fv (%) | 72 ± 1 | 83.0 ± 0.6 | 93.1 ± 0.2 | 92.8 ± 0.5 | 90.2 ± 0.4 | 51 ± 2 | … | … |
ε∞ | 1.23 ± 0.08 | 1.3 ± 0.1 | 1.5 ± 0.2 | 2.9 ± 0.1 | 1.99 ± 0.05 | 1.49 ± 0.06 | 2.02 ± 0.06 | 2.03 ± 0.07 |
Es (eV) | 7.35 ± 0.07 | 7.7 ± 0.1 | 8.1 ± 0.2 | 6.4 ± 0.1 | 7.22 ± 0.05 | 7.16 ± 0.05 | 6.69 ± 0.06 | 6.72 ± 0.07 |
As (eV2) | 23 ± 1 | 22 ± 2 | 23 ± 3 | 1.5 ± 0.5 | 17.0 ± 0.7 | 20.8 ± 0.9 | 10.5 ± 0.7 | 10.30 ± 0.08 |
Eu (eV) | 0.054 ± 0.006 | 0.054 ± 0.006 | 0.080 ± 0.007 | 0.038 ± 0.006 | 0.100 ± 0.007 | 0.04 ± 0.01 | 0.06 ± 0.02 | 0.11 ± 0.03 |
E0 (eV) | 2.430 ± 0.007 | 2.43 ± 0.02 | 2.41 ± 0.04 | 2.423 ± 0.008 | 2.39 ± 0.02 | 2.30 ± 0.06 | 2.71 ± 0.09 | 3.1 ± 0.2 |
A0 (eV−0.5) | 7.4 ± 0.4 | 5.2 ± 0.7 | 3.7 ± 0.8 | 2.6 ± 0.3 | 3.8 ± 0.3 | 3.0 ± 0.2 | 4.1 ± 0.5 | 3.9 ± 0.8 |
Γ0 (eV) | 0.13 ± 0.01 | 0.19 ± 0.02 | 0.26 ± 0.03 | 0.29 ± 0.02 | 0.37 ± 0.03 | 1.04 ± 0.08 | 1.1 ± 0.1 | 1.2 ± 0.3 |
E1-A (eV) | 5.07 ± 0.02 | 4.98 ± 0.02 | 4.92 ± 0.06 | 4.72 ± 0.06 | 4.97 ± 0.01 | 5.19 ± 0.02 | 5.12 ± 0.02 | 5.29 ± 0.06 |
A1-A (eV−0.5) | 8.6 ± 0.3 | 7.0 ± 0.2 | 6.1 ± 0.7 | 4.6 ± 0.3 | 2.0 ± 0.2 | 5.9 ± 0.2 | 5.0 ± 0.1 | 3.6 ± 0.2 |
Γ1-A (eV) | 0.98 ± 0.01 | 1.05 ± 0.02 | 1.03 ± 0.07 | 1.0 ± 0.1 | 0.23 ± 0.06 | 1.26 ± 0.02 | 1.99 ± 0.06 | 2.7 ± 0.3 |
E1-B (eV) | 5.45 ± 0.01 | 5.44 ± 0.01 | 5.39 ± 0.05 | 5.4 ± 0.1 | 5.30 ± 0.01 | 5.72 ± 0.02 | ||
A1-B (eV−0.5) | 4.6 ± 0.4 | 2.7 ± 0.3 | 2.1 ± 0.9 | 1.1 ± 0.4 | 5.8 ± 0.2 | 2.6 ± 0.3 | ||
Γ1-B (eV) | 0.22 ± 0.05 | 0.25 ± 0.07 | 0.5 ± 0.2 | 0.7 ± 0.3 | 1.22 ± 0.03 | 0.28 ± 0.08 |
Although the error associated with each fitted parameter is the primary indicator used to assess the models' sensitivity, parameter cross correlation coefficients are also examined. Some correlation coefficients are found to be somewhat high (>0.95). However, a vast majority of these cases are between two parameters that affected the model simulation in very similar ways such as ε∞ and As or fv and ds. A few instances of high CPPB parameter cross correlation are found and are almost exclusively limited to A0 and E0 correlation, likely a result of the large flexibility of lineshape in the vicinity of E0 due to the transition from Urbach to CPPB behavior. In general, the occasional correlation between parameters is a side-effect of having an optical-structural model that could be applied to the analysis of all sixteen samples while still retaining sufficient sensitivity to the fine-structure of the films' optical properties and surface structure. Models with fewer fitting parameters have been tested, but result in increased MSE and overall poorer fit quality in all cases. The combination of low MSE and reasonable error bars on all model fits reported in Table I provides justification that the presence of some cross correlation has not rendered the results and subsequent analysis unreliable. Although some parameters may be correlated, the overall resulting line shape of ε represents the characteristics of the particular CdS:O material.
With the parameterization of ε described in Equation (1), the fundamental gap energy E0 is the first allowed electronic transition and is therefore representative of the material band gap. Figure 3 shows the dependence of each sample's E0 critical point energy on oxygen gas flow ratio during sputtering. To demonstrate the reliability of using E0 as the material band gap, the band gap energies have also been determined using the absorption coefficient (α). Using ε, α for each sample is calculated using
where λ is the wavelength of incident light. Finding the zero-intercept energy of a linear fit to α2 in the region directly above the absorption onset serves as an extrapolation of each sample's direct band gap energy.21 Figure 4 shows the extrapolation over the range of α from 2.5 × 104 to 6.6 × 104 cm−1 for the 0%/270 °C/annealed sample, producing Eg = 2.43 ± 0.06 eV, which is in reasonable agreement with other published values for CdS.22–25 Similar ranges of α (∼104–105 cm−1) and, by extension, α2 are used to extrapolate Eg for all the other samples. Finally, Figure 5 shows the correspondence between E0 critical point energies and Eg values linearly extrapolated from α2. This correspondence is highlighted by the fact that a linear fit to all sixteen data points (dashed line) is extremely close to the Eg = E0 line (solid line).
Lowest critical point energy E0 for all CdS:O sample series as a function of oxygen gas flow ratio.
Lowest critical point energy E0 for all CdS:O sample series as a function of oxygen gas flow ratio.
Linear extrapolation of α2 corresponding to a range of 2.5 × 104 to 6.6 × 104 cm−1 in α for the 0%/270 °C/annealed sample to yield a band gap (Eg) of 2.43 ± 0.06 eV.
Linear extrapolation of α2 corresponding to a range of 2.5 × 104 to 6.6 × 104 cm−1 in α for the 0%/270 °C/annealed sample to yield a band gap (Eg) of 2.43 ± 0.06 eV.
Eg obtained from extrapolation of α2 to zero plotted as a function of E0. The dashed black line is a linear fit to all sixteen points.
Eg obtained from extrapolation of α2 to zero plotted as a function of E0. The dashed black line is a linear fit to all sixteen points.
Figures 3 and 5 highlight the fact that the band gap energies for the as-deposited films have relatively large variations, whereas annealing those same films results in all band gaps converging near the CdS band gap of ∼2.4 eV, regardless of oxygen gas flow ratio during deposition. A likely source of the band gap variation for the as-deposited samples is the formation of cadmium oxide (CdO) and cadmium peroxide (CdO2) compounds within the film. Numerous studies have confirmed that CdO films are readily produced using high temperatures and can have band gaps as much as a few tenths of an eV lower26–30 than pure CdS with epitaxial CdO films exhibiting a band gap as low as 2.16 eV.31 By contrast, CdO2 films are most stable near RT and feature band gaps greater than 3.3 eV and as high as 4.64 eV.30,32,33 In this context, lower E0 seen for both 1%/as-deposited samples is a likely incorporation of oxygen as in CdO. At 3% oxygen flow ratio, however, the band gaps for both of the as-deposited samples are greater than that for CdS suggesting incorporation of oxygen as in CdO2. The shift from E0 decreasing to E0 increasing occurs at lower oxygen flow ratio (2%) for RT deposited as compared to the 270 °C deposited samples (3%), which is consistent with the observation that CdO2 forms more readily at lower temperatures. Additionally, the scale of E0 deviations from the CdS value of ∼2.4 eV suggests greater CdO2-like oxygen incorporation in the RT samples, which is again consistent with the increased stability of CdO2 seen at lower temperatures. Other studies of CdS thin films have shown that increases in the microstructural tensile strain lead to increases in the band gap energy.34–38 This effect is another likely contributor to the changes in E0 observed for the as-deposited samples in Figures 3 and 5; however, studies of strain in CdS34 and in CdTe39 have demonstrated strain-induced critical point energy shifts of only up to ∼0.024 and ∼0.2 eV, respectively, meaning that this mechanism is not likely to be the dominant factor for these CdS:O films. Annealing, however, can be understood to relax the majority of microstructural strain induced by oxygen inclusion as a result of E0 being close to uniform for all annealed samples. Finally, it should be noted that the uniformity of E0 for annealed samples also suggests that performance improvements seen in CSS-deposited CdTe devices with CdS:O window layers may not be a result of increased CdS:O band gap. A more likely source of such performance improvement is the general inverse relationship between oxygen gas flow ratio and ε2 amplitude, which would allow a larger proportion of the incident light to reach the absorber layer due to greater ultraviolet transparency.
The trend of increasingly broad features in ε with increasing oxygen gas flow ratio seen in Figure 2 is in qualitative agreement with the previous reports.7–9 Figure 6 provides a more quantitative representation of how the fundamental gap transition broadening Γ0 evolves with oxygen gas flow ratio. It is noteworthy that Γ0 generally increases with increasing oxygen gas flow ratio and that for all samples Γ0 decreases after annealing. As has been previously demonstrated for CdS thin films,20 sharper critical point features (i.e., decreased broadening) are correlated with increased crystallographic order. Therefore, it can be reasonably concluded that increased oxygen gas flow ratio during sputtering generally results in increased disorder stemming from smaller grain sizes, a large defect density, or a combination of both. Additionally, as could be expected, the data suggest that both the grain size and crystallinity increase upon annealing for all samples, regardless of oxygen gas flow ratio, which is consistent with previous observations.40
Broadening of the lowest energy critical point transition (Γ0) for all CdS:O sample series as a function of oxygen gas flow ratio.
Broadening of the lowest energy critical point transition (Γ0) for all CdS:O sample series as a function of oxygen gas flow ratio.
As described earlier, ε below E0 is described by an Urbach tail where the Urbach energy Eu is generally indicative of the defect density in the material. Larger Eu results in band tails with greater absorption and further extension into the band gap. Figure 7 shows Eu as a function of E0 for each film. Despite both annealed series of films (squares and triangles) having nearly uniform E0 energies, they exhibit a spread in Eu suggesting that significant variations in defect density can persist even after annealing has modified the optical band gaps to be nearly the same for all samples. The Urbach energies of the 270 °C/annealed samples are observed to monotonically increase with oxygen gas flow ratio as opposed to the RT/annealed samples for which a clear trend is not evident. For the pure CdS samples (0% oxygen gas flow ratio), annealing can be understood to decrease the overall defect density, as is demonstrated by the decrease in Eu for both the RT and 270 °C samples upon annealing. This result is consistent with the decrease in Γ0, observed in Figure 6, and the understanding that annealing improves crystallographic order and therefore decreases defect density. In the case of the 1%–3% oxygen gas flow ratio samples, the effects of oxygen complicate the result of the annealing process since exactly half of the samples show increase in Eu while the other half shows decrease following annealing.
Urbach energy (Eu) plotted against the E0 critical point transition energy.
Finally, an analysis of the effective film thicknesses in conjunction with corresponding values of ε1 and relative material density deduced from ε1 reveals that the result of the annealing process is more complex than simple densification of the existing material in the films. Figure 8 shows the effective film thicknesses calculated as db + (1 – fv) ds and plotted as a function of oxygen gas flow ratio. Annealing is seen to result in thinner effective thicknesses for all films except for one pair where the thicknesses are within the associated error. Figure 9(a) plots the value of ε1 at 0.74 eV for all films as a function of oxygen gas flow ratio. If densification of the films is the sole cause of the thickness changes shown in Figure 8, higher values of ε1 would be expected where the films are transparent, but this behavior is observed in Figure 9 for only a few sample pairs. The film with the highest value of ε1 at 0.74 eV is identified as 0%/270 °C/as-deposited CdS. A Bruggeman effective medium approximation consisting of fractions of this relatively “dense” material and void is fit to ε1 at 0.74 eV for the other samples, with results shown in Figure 9(b). The results show a direct mirror correspondence to ε1. Consequently, the densification of existing material cannot alone explain the effect of annealing on the films. As a result of the Kramers–Kronig relationship between the real and imaginary parts of ε, the results seen in Figure 9 can be understood in the context of the other variations in ε described in this work, even variations seen in the absorbing part of the measured spectrum. The contributions from specific parameters are often difficult to deconvolute. For instance, an increase in Γ0 would result in an increase in ε1 where the film is transparent due to extension of absorption to lower photon energies. Considering the annealed and as-deposited 1%/RT pair of samples, offsetting effects on ε1 between the densification of the film as shown in Figure 8 and the decrease in Γ0 from Figure 6 could explain the exact correspondence in ε1 for that sample pair. However, similar densification and change in Γ0 are seen for the 2%/RT samples, yet they have significantly different ε1 values at 0.74 eV, indicating that a more complicated interplay between various physical mechanisms affects the overall film optical properties. Similarly, increases in E0 shifting peak absorption to higher photon energies, such as those seen in Figure 3 for the 1%/270 °C and 2%/270 °C samples as a result of annealing, can explain the corresponding decrease in ε1 at 0.74 eV. The relatively close E0 energies for the as-deposited and annealed 3%/270 °C samples could be a strong contributing factor to convergence of ε1 for those samples. However, for the 3% RT deposition samples, E0 is vastly higher for the as-deposited film when compared to its annealed counterpart while ε1 is nearly the same for both at 0.74 eV. Ultimately, multiple structural and optical characteristics of these films have been shown to be sensitive to the oxygen inclusion but no single parameter dominates the optical response for all films. Further study will be necessary to more comprehensively understand the exact role oxygen plays in the composition of CdS:O films.
Effective film thickness, calculated as db + (1 – fv) ds, plotted as a function of oxygen gas flow ratio.
Effective film thickness, calculated as db + (1 – fv) ds, plotted as a function of oxygen gas flow ratio.
(a) ε1 at E = 0.74 eV for all films plotted as a function of oxygen gas flow ratio. (b) Relative void fraction extracted using a Bruggeman effective medium approximation consisting of variable fractions of void (fv) and 0%/270 °C/as-deposited CdS:O.
(a) ε1 at E = 0.74 eV for all films plotted as a function of oxygen gas flow ratio. (b) Relative void fraction extracted using a Bruggeman effective medium approximation consisting of variable fractions of void (fv) and 0%/270 °C/as-deposited CdS:O.
CONCLUSIONS
Spectroscopic ellipsometry has been used to study the effects on spectra in ε obtained for CdS:O thin films for multiple combinations of oxygen volumetric gas flow ratios from 0% to 3% during sputtering, RT and 270 °C deposition temperatures, and 607 °C high-temperature annealing similar to temperatures found in CSS of CdTe. As expected, ε of films deposited at 0% oxygen gas flow ratio most closely resemble ε of CdS published elsewhere while the critical point features of films with increasing oxygen flow ratio are increasingly broadened. The band gap energies of as-deposited films are sensitive to relative oxygen gas flow ratio during deposition, whereas all annealed films exhibit band gaps resembling that of CdS. In the broader context of full solar cell devices, our results indicate that the optimum fabrication conditions for CdS:O layers will likely differ for different types of PV devices. For instance, only the annealed samples in this study are relevant to CdTe superstrate cells since the high temperature CdTe deposition will follow the CdS:O deposition. For such devices, the most promising candidate may be the 3%/RT/annealed CdS:O since it has the best combination of increased crystallinity as assessed by narrow broadening of the lowest energy critical point, low sub-gap absorption represented by the Urbach energy, and low above-gap absorption aiding in ultraviolet transparency. It is likely that performance gains observed in CdTe solar cells through the use of CdS:O window layers are the result of the desirable characteristics previously mentioned and not the increased bandgap in the CdS:O layers as initially believed.
ACKNOWLEDGMENTS
This work was supported by University of Toledo start-up funds, the Ohio Department of Development (ODOD) Ohio Research Scholar Program (Northwest Ohio Innovators in Thin Film Photovoltaics, Grant No. TECH 09-025), National Science Foundation (CBET-1230246), and Office of Naval Research (11847944).