Next Article in Journal
Multi-Ferroic Properties on BiFeO3/BaTiO3 Multi-Layer Thin-Film Structures with the Strong Magneto-Electric Effect for the Application of Magneto-Electric Devices
Previous Article in Journal
Meso-Simulation and Experimental Research on the Mechanical Behavior of an Energetic Explosive
 
 
Font Type:
Arial Georgia Verdana
Font Size:
Aa Aa Aa
Line Spacing:
Column Width:
Background:
Article

Effect of Electric Field Regulation on Laser Damage of Composite Low-Dispersion Mirrors

1
Laboratory of Thin Film Optics, Shanghai Institute of Optics and Fine Mechanics, Shanghai 201800, China
2
Center of Materials Science and Optoelectronics Engineering, University of Chinese Academy of Sciences, Beijing 100049, China
3
Key Laboratory of Material for High Power Laser, Shanghai Institute of Optics and Fine Mechanics, Shanghai 201800, China
4
State Key Laboratory of High Field Laser Physics, Shanghai Institute of Optics and Fine Mechanics, Shanghai 201800, China
5
CAS Center for Excellence in Ultra-Intense Laser Science, Shanghai 201800, China
6
Hangzhou Institute for Advanced Study, Hangzhou 310024, China
*
Authors to whom correspondence should be addressed.
Coatings 2021, 11(1), 65; https://doi.org/10.3390/coatings11010065
Submission received: 1 December 2020 / Revised: 13 December 2020 / Accepted: 5 January 2021 / Published: 8 January 2021

Abstract

:
Low dispersion mirrors are important because of their potential use in petawatt (PW) laser systems. The following two methods are known to increase the laser-induced damage threshold of low dispersion optical components: use of a wide-bandgap-material protective layer and control of electric field distribution. By controlling the electric field distribution of composite low-dispersion mirrors (CLDM), we shift the electric field peaks from the material interface into the wide-bandgap material. However, the damage threshold of modified-electric-field composite low dispersion mirror (E-CLDM) does not increase. Damage morphology shows that the initial damaged layer is Ta2O5. An immediate cause is the enhancement of the electric field in internal layers caused by surface electric field regulation. Theoretical calculations show that the damage threshold of CLDM or E-CLDM is determined by the competition results of bandgap and the electric field of layer materials. The CLDM with different materials or different protective layer periods can be optimally designed according to the electric field competition effect in the future.

1. Introduction

The development of high-power petawatt (PW) laser promotes the development of physics, medicine, biology and materials science [1,2,3,4,5]. However, the generation of high-power pulses is constrained by the laser-induced damage threshold (LIDT) of optical elements. In particular, the LIDT of a low-dispersion mirror (LDM) is a weak point in the development of high-power ultrafast systems [6]. LDMs that can afford a broadband high-reflection (HR) spectrum, high LIDT, and stable group delay dispersion (GDD) play an essential role for PW lasers with pulses in the femtosecond regime [7]. However, reflection bandwidth, dispersion and damage threshold are interdependent, restricting each other [8]. Thereby, the LIDT of broad-bandwidth, low-dispersion mirrors have become a recognized research focus [8,9,10,11,12,13,14,15,16].
Quarter-wave optical thickness (QWOT) mirrors are the most commonly used low dispersion mirrors. The current work to raise the threshold is based on QWOT mirrors. Therefore, how to raise the threshold without sacrificing bandwidth and dispersion is very meaningful. Several researchers have reported experimental results for LDMs [17]. Such studies on a large number of samples are known [16,18]. Several methods are recognized to be effective in increasing the threshold of QWOT [19]. The first method is to increase the damage resistance by using wide-bandgap-material protective layers. Depositing a highly damaged resistant layer stack on a conventional quarter-wave mirror (composite low dispersion mirrors, CLDM) overcomes the tradeoff between LIDT and bandwidth. Takada et al. proposed a broadband mirror with high damage fluence for chirped-pulsed amplification of 10 fs pulses. This mirror consists of broadband TiO2/SiO2 coatings and optimized high-damage-threshold ZrO2/SiO2 coatings [7]. Patel et al. demonstrated that a modified Ta2O5/SiO2 structure in which the high index layer is replaced by either HfO2 or Y2O3 for the three uppermost high-index layers results in an increase of ~50% in LIDT when measured at 1 μm using 350 ps laser pulses [15]. The second method to increase the damage threshold is electric field regulation. According to previous research, the damage caused to optical elements occurs at a laser power that yields a critical electric field intensity in the coating material [20]. Apfel et al. derived a mirror structure with thinner high-index layers, reducing the peak electric field in the high-index material by 33% and shifting the peak electric field away from the interface [21]. Bellum et al. used a similar method, where at an angle of incidence of 45° both the threshold of s- and p-polarization increased. [13]. Schiltz et al. observed that a modified-electric-field composite low dispersion mirror (E-CLDM) does not offer any definite damage performance advantages over the standard CLDM when tested for a 4 ns source and a 0.19 ns source [11]. However, the reason was not given in his report.
Compared with QWOT, the CLDM can increase the threshold without sacrificing the bandwidth by using wide-bandgap-material protective layers, and the method of electric field regulation can shift the peak electric field to the low-index material. Furthermore, the damage threshold in the femtosecond regime is more dependent on the electric field [12]. Therefore, we believe that combining the two methods can further increase the threshold in the femtosecond regime.

2. Materials, Design and Methods

We aim to design high-damage-threshold mirrors that meet a minimum reflectivity of 99.5% at a 45° incidence angle for p-polarization with GDD < ±300 fs2 over a spectral range of 750–850 nm. We choose SiO2 as a low-index material (~1.46), which is well-known for exhibiting high resistance to femtosecond laser damage. And Ta2O5 and Al2O3 is as a high-index material. In this study, we choose Al2O3 as the top high-index material which has a wide bandgap of 6.5 eV. The layer stack is represented by the formula G|(HL)m (XL)n−1X|Air, where m is the periods of Ta2O5/SiO2 stack; n is the periods of Al2O3 layer, and H, L, and X denote Ta2O5, SiO2, and Al2O3, respectively, G is substrate.
Figure 1a shows the calculated electric field distribution of CLDM for different protective layers. As the number of Al2O3 periods increases, the electric field in the narrow-bandgap material decreases. Meanwhile, the peak electric field intensity in Al2O3 remains constant. To ensure that the protective layer work, we need as many protective layers (Al2O3) as possible. However, different periods of the Al2O3 protective layer significantly impact the GDD performance, as shown in Figure 2a. The calculated GDDs of CLDM and E-CLDM are obtained by the film design software TFCalc. As the number of Al2O3 periods increases, GDD increases. When the number of periods n is 5, the maximum GDD ripple is just under ±300 fs2. Considering the electric field and dispersion, we replace Ta2O5 with Al2O3 in the five uppermost high-index layers. The layer stack is represented by the formula G|HL)16(XL)4X|Air. The initial design is a Ta2O5-Al2O3/SiO2 composite mirror with 41 layers. This design combines the superior optical properties of Ta2O5 and the higher damage threshold of Al2O3. The layer structure of the quarter-wave optical-thickness composite mirror is shown in Figure 3a and the electric field intensity distribution in the proximity of the Ta2O5-Al2O3 interface is shown in Figure 1a (n = 5). The electric field distribution shows that the peaks’ electric fields are located at the material interfaces, which can easily lead to damage, and that the maximum field intensities at the Al2O3 and Ta2O5 interfaces are 1.2 and 0.33, respectively.
The design E-CLDM, based on the initial design, is optimized such that the electric field is shifted away from the material interfaces and into the low-index high-damage threshold material (SiO2). The electric field distribution of E-CLDM for different n is shown in Figure 1b. We keep the electric field in Al2O3 and SiO2 constant for different n. As the number of Al2O3 periods increases, the electric field in the Ta2O5 decreases. However, compared with the electric field in CLDM, the electric field in Ta2O5 of E-CLDM is higher. The layer profile of E-CLDM (n = 5) is shown in Figure 3b. It is obvious that the thickness of the Al2O3 is decreased, while that of the low-index material is increased [21]. The electric field distribution is shown in Figure 1b (n = 5), where the electric field intensity peaks are located in the low-index material and the maximum field intensities in Al2O3, SiO2 and Ta2O5 are 0.8 and 0.55, respectively. At the same time, the maximum electric field intensity in SiO2 increases to 1.35.
Figure 2a,b shows a comparison between the theoretical GDD of the CLDM and E-CLDM stacks. For n = 5, the dispersion curve of E-CLDM exhibits a protrusion over the spectral range 750–760 nm, but still meets the design requirements in the working band (750–850 nm). The modified design has superior dispersion value of ±175 fs2, compared to the value of ±300 fs2 for the CLDM stack. However, for n > 5, neither CLDM nor E-CLDM meets the requirements of dispersion.

3. Fabrication

Mirrors based on Figure 3a,b were fabricated by dual-ion-beam sputtering technique (Spector, Veeco) with two ion sources (16 cm main source and 12 cm assistant source). The high-energy argon ions produced by 16 cm main source bombard the target (Ta, Al, SiO2). The main function of the 12 cm assistant ion source is the pre-cleaning of the substrate and the improvement the coating absorption, making the coating more dense and bonding with the substrate stronger. The background pressure is 10−4 Pa and the substrate baking temperature is 120 °C.

4. Results

4.1. Reflectivity

The reflection spectrum was measured with a Perkin–Elmer (Lambda 1050) spectrophotometer. The reflectivities of the two sample types for p-polarization at 45° AOI are shown in Figure 4. This is consistent with that expected for the E-CLDM stack, which performs similarly to the CLDM stack. Both E-CLDM and CLDM stacks provide a reflectivity of 99.5% over a spectral range of 750–850 nm.

4.2. Damage Threshold

A laser damage test for two types of samples was performed in the 1-on-1 mode [22]. Pulses were generated by a Ti:sapphire laser system with an 800 nm central wavelength and a pulse duration of 30 fs, and were p-polarized and incident at 45°. The spectral range is 800 (±35 nm). The measurement spot area is 0.221 mm2 and the error range is 3%. The experimental setup is shown in Figure 5. A CCD camera was used to observe the damage in real time.
Firstly, we measured the damage threshold of three low-dispersion mirrors, including CLDM, E-CLDM and 41 layers quarter-wave optical thickness mirror (Ta2O5/SiO2), as shown in Figure 6. Compared to QWOT, which comprises a Ta2O5/SiO2 stack and has a low damage threshold of 0.32 J/cm2, the damage threshold was increased by 50% to 0.48 J/cm2 for CLDM. However, contrary to our expectations, the damage threshold of E-CLDM was found to be lower than that of CLDM at only 0.41 J/cm2. In other words, electric field regulation did not increase the damage threshold of the composite mirror. However, the damage thresholds of both CLDM and E-CLDM were higher than that of QWOT.

4.3. Damage Morphology

To explain why electric field regulation would decrease the damage threshold of a composite mirror, the damage morphology of the E-CLDM stack was observed by scanning electron microscopy. As shown in Figure 7, the SEM results suggest that while the initial damage morphology (Figure 7a) occurred at a laser pulse fluence of 0.43 J/cm2, the other two damage morphologies (Figure 7c,d) occurred at higher fluences. The beam is incident obliquely from the right side of the picture. Firstly, at a laser fluence of 0.43 J/cm2, an inner layer material was melted and gasified, and the resulting gas pressure deformed the outer layer, forming a protrusion. At a fluence of 0.45 J/cm2, the internal pressure exceeded the limit stress of the layer, and thus, damaged the protrusion structure. As the fluence was further increased to 0.5 J/cm2, the bulge structure was detached and exposed to a damage pit.
To demonstrate the initial damage layer, we further observed the cross-sectional morphology after focused-ion-beam sectioning. The cross-sectional morphology of region 1 of the protrusion is shown in Figure 7d and the diagrammatic sketch of Figure 7d is shown in Figure 7e. Because the atomic number of Al is close to that of Si, the Al2O3/SiO2 stack layer cannot be clearly observed. However, the first Al2O3 layer and Ta2O5 layer can be observed. A precise measurement shows that the distance between the first Al2O3 layer and the Ta2O5 layer is 1535 nm, and the design distance is 1542 nm. These data suggest that the position of the layer is accurate. The white layers are Ta2O5 and black layers are SiO2.
It is unexpected that the initial damage site is located in the Ta2O5 layer. Taken together, these results suggest that the wide-bandgap material Al2O3 has no protective effect on the narrow-bandgap material Ta2O5. This causes the damage threshold of E-CLDM to be lower than that of CLDM.

5. Discussion

We next consider why the initial damage layer is Ta2O5. The threshold values presented in Section 4.2 were calculated without considering the electric field distribution. If the distribution is considered, internal thresholds that are characteristic for the layers will be obtained. Therefore, if the initial damage layer for different coatings is made of the same material, we can calculate the relations among damage thresholds of different designs from the electric field distribution. Thus, the theoretical damage threshold can be calculated according to Equation (1) [16,23].
F t = F i n t × E i n c 2 / E m a x 2
Here F t is the theoretical damage threshold of the front surface of the sample, F i n t is the internal threshold of layer X, E i n c is the magnitude of the incident electric field, and E m a x is the magnitude of the electric field inside layer X.
The internal threshold of a Ta2O5 layer can be calculated from the damage threshold of Ta2O5/SiO2, as shown in Figure 6. The damage threshold of SiO2 and Al2O3 layers can be obtained from the previous work of our group [24,25]. Thus, the internal thresholds of Ta2O5, Al2O3, and SiO2 layers are 0.101, 0.337, and 0.430 J/cm2, respectively. Figure 8 shows theoretical damage thresholds of CLDM or E-CLDM with different numbers of Al2O3 periods. The threshold of CLDM or E-CLDM is decided by the lowest threshold value in layer materials.
From Figure 8a, a competitive relationship exists between Ta2O5 and SiO2 in CLDM. We find that the threshold in Ta2O5 layer increases with the number of Al2O3 layer periods, because at different Al2O3 periods, the electric field in Ta2O5 decreases as shown in Figure 1b. So, if n < 5, the threshold in Ta2O5 layer is always the lowest value, that is, the damage source is in internal layer Ta2O5. In the case of n = 5 or n > 5, the electric field in Ta2O5 is at a very low level resulting in the threshold in Ta2O5 exceeds that in Al2O3. The damage source is in surface Al2O3 layer. The electric field distribution of E-CLDM for different n is shown in Figure 1b. Compared with the electric field intensity of Ta2O5 in CLDM, the stack of E-CLDM has a higher intensity in Ta2O5. It implies that the surface electric field regulation causes the enhancement of the electric field in narrow band material Ta2O5. The threshold of E-CLDM with different numbers of Al2O3 periods is shown in Figure 8b. Compared with Figure 8a, the competitive relationship exists between Ta2O5 and SiO2. If n < 9, the threshold of E-CLDM decreased because of the enhancement of the electric field in Ta2O5. n = 9 is an inflection point and the electric field in Ta2O5 is at a low level resulting in the threshold in Ta2O5 layer exceeds that of SiO2. In the case of n > 9, the damage source is in SiO2, and the threshold of E-CLDM keeps constant. So the optimal n for E-CLDM is 9. The threshold of E-CLDM for n > 9 has no significant increase compared with CLDM. And considering the GDD, n = 9 is not a good choice. In summary, the method of shifting the electric field to wide-bandgap-material is no longer suitable for CLDM.
The competition effect can help us to obtain the best electric field control results for CLDM with different material combinations and different protective layer periods. We need to control the electric field according to the competition results of bandgap and the electric field of layer materials.
According to the electric field distribution shown in Figure 1 (n = 5), we calculate the theoretical threshold in Ta2O5, Al2O3, and SiO2 layers of E-CLDM are 0.50, 1.20, and 0.84 J/cm2, respectively. Clearly, the theoretical threshold of E-CLDM is 0.50 J/cm2 and the initial damage layer is Ta2O5. The measured threshold is 0.41 J/cm2. These data are consistent with the cross-sectional morphology, as shown in Figure 7d. Similarly, the theoretical thresholds in Ta2O5, Al2O3, and SiO2 layer of CLDM for n = 5 are 0.86, 0.78, and 0.94 J/cm2. The theoretical threshold of CLDM is 0.78 J/cm2 and the measured threshold is 0.48 J/cm2. Both the calculated damage thresholds are higher than the corresponding experimental thresholds. We attribute this discrepancy to low adhesion at the layer interfaces and residual stress that lower the threshold.
The internal threshold of Al2O3 is calculated through a single Al2O3 layer and that of Ta2O5 is calculated through Ta2O5/SiO2. So this is the reason why there is a large deviation between the calculated result of CLDM and the experimental result. The relation between the calculated damage thresholds of the two samples (CLDM and E-CLDM) agrees with the experimental results.

6. Conclusions

In summary, we combined the methods of electric field regulation and wide-bandgap protective layers in the femtosecond regime. The damage threshold of two types of composite low-dispersion mirrors, with and without electric field regulation, are investigated using femtosecond laser pulses. The results show that the damage threshold of E-CLDM is lower than that of CLDM. The internal threshold is used to calculate the theoretical threshold of all samples. The damage threshold of CLDM or E-CLDM is determined by the competition results of bandgap and the electric field. The damage properties of layer materials are determined by bandgap and electric field distribution. The theoretical results show that the enhancement of the electric field in internal layers, caused by surface electric field regulation, is an immediate cause of the threshold to decrease. These data suggest that the method of shifting the electric field to wide-bandgap-material is no longer suitable for CLDM. The competitive effect between layer materials must be considered in the new electric field modulation method. The competition effect can help us to obtain the best electric field control results for CLDM with different material combinations and different protective layer periods. This study contributes to finding new ways to improve the LIDT of low-dispersion mirrors.

Author Contributions

Conceptualization: Y.W., J.S.; Data curation: Y.Z. (Yuhui Zhang), R.C.; Formal analysis: Y.Z. (Yuhui Zhang); Investigation, Y.Z. (Yuhui Zhang), Z.W.; Project administration: Y.W., H.H., D.L., Y.Z. (Yuanan Zhao), Y.J., K.Y., Y.S., Y.L., R.L. and J.S.; Validation: M.Z. and Y.J.; Writing—original draft: Y.Z. (Yuhui Zhang); Writing—review & editing: Y.W. All authors have read and agreed to the published version of the manuscript.

Funding

This work was supported by National Key R&D program of China (2018YFE0118000), Research on the Key Technology of TMT Large Aperture Wide Angle Spectral Dichroic Mirror (U1831211); the National Natural Science Foundation of China (Grant No. 11904376), NSAF Fund Jointly set up by the National Natural Science Foundation of China and the Chinese Academy of Engineering Physics (No. U1630140), the Youth Innovation Promotion Association, Chinese Academy of Sciences (CAS) (2017289), and the Strategic Priority Research Program of CAS (Grant No. XDB1603).

Informed Consent Statement

Informed consent was obtained from all subjects involved in the study.

Data Availability Statement

The data presented in this study are available on request from the corresponding author. The data are not publicly available due to privacy and secret.

Conflicts of Interest

The authors declare no conflict of interest.

References

  1. Li, W.; Gan, Z.; Yu, L.; Wang, C.; Liu, Y.; Guo, Z.; Xu, L.; Xu, M.; Hang, Y.; Xu, Y.; et al. 339 J high-energy Ti:sapphire chirped-pulse amplifier for 10 PW laser facility. Opt. Lett. 2018, 43, 5681–5684. [Google Scholar] [CrossRef] [PubMed]
  2. Skobelev, I.Y.; Ryazantsev, S.N.; Arich, D.D.; Bratchenko, P.S.; Faenov, A.Y.; Pikuz, T.A.; Durey, P.; Doehl, L.; Farley, D.; Baird, C.D.; et al. X-ray absorption spectroscopy study of energy transport in foil targets heated by petawatt laser pulses. Photonics Res. 2018, 6, 234–237. [Google Scholar] [CrossRef]
  3. Danson, C.N.; Haefner, C.; Bromage, J.; Butcher, T.; Chanteloup, J.-C.F.; Chowdhury, E.A.; Galvanauskas, A.; Gizzi, L.A.; Hein, J.; Hillier, D.I.; et al. Petawatt and exawatt class lasers worldwide. High Power Laser Sci. Eng. 2019, 7, e54. [Google Scholar] [CrossRef]
  4. Liang, X.; Xie, X.; Kang, J.; Yang, Q.; Wei, H.; Sun, M.; Zhu, J. Design and experimental demonstration of a high conversion efficiency OPCPA pre-amplifier for petawatt laser facility. High Power Laser Sci. Eng. 2018, 6, 58. [Google Scholar] [CrossRef] [Green Version]
  5. Turcu, I.C.E.; Shen, B.; Neely, D.; Sarri, G.; Tanaka, K.A.; McKenna, P.; Mangles, S.P.D.; Yu, T.-P.; Luo, W.; Zhu, X.-L.; et al. Quantum electrodynamics experiments with colliding petawatt laser pulses. High Power Laser Sci. Eng. 2019. [Google Scholar] [CrossRef] [Green Version]
  6. Angelov, I.B.; Von Conta, A.; Trushin, S.A.; Major, Z.; Karsch, S.; Krausz, F.; Pervak, V. Investigation of the Laser-Induced Damage of Dispersive Coatings; SPIE Laser Damage: Boulder, CO, USA, 2011. [Google Scholar]
  7. Takada, H.; Kakehata, M.; Torizuka, K. Broadband high-energy mirror for ultrashort pulse amplification system. Appl. Phys. A 2000, 70, S189–S192. [Google Scholar] [CrossRef]
  8. Chen, R.; Wang, Y.; Guo, K.; Zhu, M.; Yi, K. Design, fabrication and laser damage comparisons of low-dispersive mirrors. In Proceedings of the Pacific Rim Laser Damage 2019: Optical Materials for High-Power Lasers, Qingdao, China, 19–22 May 2019. [Google Scholar]
  9. Oliver, J.B.; Bromage, J.; Smith, C.; Sadowski, D.; Dorrer, C.; Rigatti, A.L. Plasma-ion-assisted coatings for 15 femtosecond laser systems. Appl. Opt. 2014, 53, A221–A228. [Google Scholar] [CrossRef] [PubMed]
  10. Bellum, J.C.; Winstone, T.B.; Field, E.S.; Kletecka, D.E. Broad Bandwidth High Reflection Coatings for Petawatt Class Lasers: Femtosecond Pulse Laser Damage Tests, and Measurement of Group Delay Dispersion; SPIE Laser Damage: Boulder, CO, USA, 2017. [Google Scholar]
  11. Schiltz, D.; Patel, D.; Baumgarten, C.; Reagan, B.A.; Rocca, J.J.; Menoni, C.S. Strategies to increase laser damage performance of Ta2O5/SiO2 mirrors by modifications of the top layer design. Appl. Opt. 2017, 56, 136–139. [Google Scholar] [CrossRef] [PubMed]
  12. Velpula, P.K.; Ďurák, M.; Kramer, D.; Meadows, A.R.; Vilémová, M.; Rus, B. Evolution of femtosecond laser damage in a hafnia-silica multi-layer dielectric coating. Opt. Lett. 2019, 44, 5342–5345. [Google Scholar] [CrossRef] [PubMed]
  13. Bellum, J.C.; Field, E.S.; Winstone, T.B.; Kletecka, D.E. Low Group Delay Dispersion Optical Coating for Broad Bandwidth High Reflection at 45° Incidence, P Polarization of Femtosecond Pulses with 900 nm Center Wavelength. Coatings 2016, 6, 11. [Google Scholar] [CrossRef] [Green Version]
  14. Hervy, A.; Gallais, L.; Chériaux, G.; Mouricaud, D. Femtosecond laser-induced damage threshold of electron beam deposited dielectrics for 1-m class optics. Opt. Eng. 2016, 56, 011001. [Google Scholar] [CrossRef] [Green Version]
  15. Patel, D.; Schiltz, D.; Langton, P.F.; Emmert, L.; Acquaroli, L.N.; Baumgarten, C.; Reagan, B.; Rocca, J.J.; Rudolph, W.; Markosyan, A.; et al. Improvements in the Laser Damage Behavior of Ta2O5/SiO2 Interference Coatings by Modification of The Top Layer Design; SPIE Laser Damage: Boulder, CO, USA, 2013. [Google Scholar]
  16. Angelov, I.B.; Von Pechmann, M.; Trubetskov, M.; Krausz, F.; Pervak, V. Optical breakdown of multilayer thin-films induced by ultrashort pulses at MHz repetition rates. Opt. Express 2013, 21, 31453–31461. [Google Scholar] [CrossRef] [PubMed] [Green Version]
  17. Velpula, P.K.; Kramer, D.; Rus, B. Femtosecond Laser-Induced Damage Characterization of Multilayer Dielectric Coatings. Coatings 2020, 10, 603. [Google Scholar] [CrossRef]
  18. Negres, R.A.; Stolz, C.J.; Kafka, K.R.P.; Chowdhury, E.A.; Kirchner, M.; Shea, K.; Daly, M. 40-fs Broadband Low Dispersion Mirror Thin Film Damage Competition; SPIE Laser Damage: Boulder, CO, USA, 2016. [Google Scholar]
  19. Jupé, M.; Lappschies, M.; Jensen, L.; Starke, K.; Melninkaitis, A.; Sirutkaitis, V.; Cravetchi, I.; Rudolph, W. Mixed Oxide Coatings for Advanced Fs-Laser Applications; SPIE Laser Damage: Boulder, CO, USA, 2007. [Google Scholar]
  20. Apfel, J.H.; Matteucci, J.S.; Newnam, B.E.; Gill, D.H. The Role of Electric Field Strength in Laser Damage of Dielectric Multilayers. NBS Spec. Publ. 1976, 462, 301. [Google Scholar]
  21. Apfel, J.H. Optical coating design with reduced electric field intensity. Appl. Opt. 1977, 16, 1880–1885. [Google Scholar] [CrossRef] [PubMed]
  22. International Organization for Standardization. ISO 21254-1:2000 (E), Laser and Laser-Related Equipment—Determination of Laser-Induced Damage Threshold of Optical Surfaces—Part 1: 1-on-1 Test; International Organization for Standardization: Geneva, Switzerland, 2000. [Google Scholar]
  23. Hervy, A.; Gallais, L.; Mouricaud, D.; Chériaux, G.; Utéza, O.; Clady, R.; Sentis, M.; Freneaux, A. Thin Films Characterizations to Design High-Reflective Coatings for Ultrafast High Power Laser Systems; SPIE Laser Damage: Boulder, CO, USA, 2014. [Google Scholar]
  24. Li, Z.; Du, J.; Zhao, Y.; Wang, Y.; Leng, Y.; Shao, J. Modeling the effect of nanosecond laser conditioning on the femtosecond laser-induced damage of optical films. Opt. Express 2015, 23, 14774–14783. [Google Scholar] [CrossRef] [PubMed]
  25. Li, Z.H. Research on the Mechanisms in Ultra-Fast Nonlinear Laser-Induced Damage in Optical Coatings. Master’s Thesis, University of Chinese Academy of Sciences, Beijing, China, 2015. (In Chinese). [Google Scholar]
Figure 1. Calculated electric field distribution for different numbers of protective layer periods. (a) The electric field of a composite low-dispersion mirror (CLDM) for different numbers of protective layer periods. As the number of Al2O3 periods increases, the electric field in the narrow-bandgap material decreases. Meanwhile, the peak electric field intensity in Al2O3 remains constant. (b) The electric field of E-CLDM for different numbers of protective layer periods.
Figure 1. Calculated electric field distribution for different numbers of protective layer periods. (a) The electric field of a composite low-dispersion mirror (CLDM) for different numbers of protective layer periods. As the number of Al2O3 periods increases, the electric field in the narrow-bandgap material decreases. Meanwhile, the peak electric field intensity in Al2O3 remains constant. (b) The electric field of E-CLDM for different numbers of protective layer periods.
Coatings 11 00065 g001
Figure 2. Dispersion for different numbers of protective layer periods. (a) CLDM, when n = 5, the maximum group delay dispersion (GDD) ripple is just under ±300 fs2. When n > 5, the GDD ripple does not meet the requirements; (b) E-CLDM, when n = 5, the modified design has a superior dispersion value of ±175 fs2, compared to the value of ±300 fs2 for the CLDM stack. However, for n > 5, the GDD ripple does not meet the requirements.
Figure 2. Dispersion for different numbers of protective layer periods. (a) CLDM, when n = 5, the maximum group delay dispersion (GDD) ripple is just under ±300 fs2. When n > 5, the GDD ripple does not meet the requirements; (b) E-CLDM, when n = 5, the modified design has a superior dispersion value of ±175 fs2, compared to the value of ±300 fs2 for the CLDM stack. However, for n > 5, the GDD ripple does not meet the requirements.
Coatings 11 00065 g002
Figure 3. (a,b) Layer thickness profile of a CLDM stack of Ta2O5-Al2O3/SiO2 (a) and that of a layer stack of Ta2O5-Al2O3/SiO2 with reduced electric field intensity inside the Al2O3 layers.
Figure 3. (a,b) Layer thickness profile of a CLDM stack of Ta2O5-Al2O3/SiO2 (a) and that of a layer stack of Ta2O5-Al2O3/SiO2 with reduced electric field intensity inside the Al2O3 layers.
Coatings 11 00065 g003
Figure 4. Measured and designed reflectivity of CLDM (a) and modified-electric-field CLDM (E-CLDM) (b) for p-polarization of 45° AOI.
Figure 4. Measured and designed reflectivity of CLDM (a) and modified-electric-field CLDM (E-CLDM) (b) for p-polarization of 45° AOI.
Coatings 11 00065 g004
Figure 5. Experimental setup used for laser damage test.
Figure 5. Experimental setup used for laser damage test.
Coatings 11 00065 g005
Figure 6. Damage threshold results for quarter-wave optical thickness (QWOT), CLDM, and E-CLDM. The thresholds of QWOT, CLDM and E-CLDM are 0.32, 0.48 and 0.41 J/cm2, respectively. EFI—electric field intensity; Fluence—radiant energy per unit area.
Figure 6. Damage threshold results for quarter-wave optical thickness (QWOT), CLDM, and E-CLDM. The thresholds of QWOT, CLDM and E-CLDM are 0.32, 0.48 and 0.41 J/cm2, respectively. EFI—electric field intensity; Fluence—radiant energy per unit area.
Coatings 11 00065 g006
Figure 7. (ac) surface damage morphology of E-CLDM at different fluences; (d) cross-sectional morphology of region 1 of the protrusion shown in (a); (e) diagrammatic sketch of (d). At a laser fluence of 0.43 J/cm2, an inner layer material was melted and gasified, and the resulting gas pressure deformed the outer layer, forming a protrusion. At a fluence of 0.45 J/cm2, the internal pressure exceeded the limit stress of the layer, and thus, damaged the protrusion structure. As the fluence was further increased to 0.5 J/cm2, the bulge structure was detached and exposed to a damage pit. The real thickness of Al2O3/SiO2 stack is consistent with the design thickness. The initial damage layer is located in the Ta2O5 layer.
Figure 7. (ac) surface damage morphology of E-CLDM at different fluences; (d) cross-sectional morphology of region 1 of the protrusion shown in (a); (e) diagrammatic sketch of (d). At a laser fluence of 0.43 J/cm2, an inner layer material was melted and gasified, and the resulting gas pressure deformed the outer layer, forming a protrusion. At a fluence of 0.45 J/cm2, the internal pressure exceeded the limit stress of the layer, and thus, damaged the protrusion structure. As the fluence was further increased to 0.5 J/cm2, the bulge structure was detached and exposed to a damage pit. The real thickness of Al2O3/SiO2 stack is consistent with the design thickness. The initial damage layer is located in the Ta2O5 layer.
Coatings 11 00065 g007
Figure 8. (a) Theoretical damage thresholds for all layer materials of CLDM with different protective layer periods. The threshold in Ta2O5 increases with the number of Al2O3 periods and the actual threshold of CLDM has the lowest threshold value for layer materials. n = 5 is an inflection point. n < 5, the damage threshold of E-CLDM increases with the n increasing; n > 5, the threshold of CLDM remains unchanged. (b) Theoretical damage thresholds for all layer materials of E-CLDM with different protective layer periods. n = 9 is an inflection point. n < 9, the damage source is in Ta2O5. n > 9, the damage source is in SiO2 and the threshold of E-CLDM keep constant.
Figure 8. (a) Theoretical damage thresholds for all layer materials of CLDM with different protective layer periods. The threshold in Ta2O5 increases with the number of Al2O3 periods and the actual threshold of CLDM has the lowest threshold value for layer materials. n = 5 is an inflection point. n < 5, the damage threshold of E-CLDM increases with the n increasing; n > 5, the threshold of CLDM remains unchanged. (b) Theoretical damage thresholds for all layer materials of E-CLDM with different protective layer periods. n = 9 is an inflection point. n < 9, the damage source is in Ta2O5. n > 9, the damage source is in SiO2 and the threshold of E-CLDM keep constant.
Coatings 11 00065 g008
Publisher’s Note: MDPI stays neutral with regard to jurisdictional claims in published maps and institutional affiliations.

Share and Cite

MDPI and ACS Style

Zhang, Y.; Wang, Y.; He, H.; Chen, R.; Wang, Z.; Li, D.; Zhu, M.; Zhao, Y.; Jin, Y.; Yi, K.; et al. Effect of Electric Field Regulation on Laser Damage of Composite Low-Dispersion Mirrors. Coatings 2021, 11, 65. https://doi.org/10.3390/coatings11010065

AMA Style

Zhang Y, Wang Y, He H, Chen R, Wang Z, Li D, Zhu M, Zhao Y, Jin Y, Yi K, et al. Effect of Electric Field Regulation on Laser Damage of Composite Low-Dispersion Mirrors. Coatings. 2021; 11(1):65. https://doi.org/10.3390/coatings11010065

Chicago/Turabian Style

Zhang, Yuhui, Yanzhi Wang, Hongbo He, Ruiyi Chen, Zhihao Wang, Dawei Li, Meiping Zhu, Yuanan Zhao, Yunxia Jin, Kui Yi, and et al. 2021. "Effect of Electric Field Regulation on Laser Damage of Composite Low-Dispersion Mirrors" Coatings 11, no. 1: 65. https://doi.org/10.3390/coatings11010065

Note that from the first issue of 2016, this journal uses article numbers instead of page numbers. See further details here.

Article Metrics

Back to TopTop