2 Post-compression after a standard compressor

Traditional post-compression for high peak power lasers with a standard compressor (L ₁ = L ₂) is shown in Figure 1. The compressed laser beam is firstly spectrally broadened through nonlinear transmission in thin plates (TTPs), and then dispersion compensated by chirped mirrors (CMs).

Figure 1 Setup of post-compression in high peak power lasers with a standard compressor (G ₁, G ₂, G ₃ and G ₄, L ₁ = L ₂) and an AFGC ( ${G}_1^{\prime }$ , G ₂, G ₃ and ${G}_4^{\prime }$ , L ₁ ≠ L ₂).

Assuming that the pulse spectrum (ranging from 750 to 850 nm) is 60 nm full width at half maximum (FWHM), the pulse duration is ${\tau}_{\mathrm{FWHM}}=30\;\mathrm{fs}$ , the spatial beam fluence is a 10th super-Gaussian distribution and the spatial noise is a sinusoidal distribution for simplicity. Its corresponding maximal peak intensity in numerical simulations is about 2.8 TW/cm². These parameters are set with reference to our SULF-1 PW laser beamline^[ Reference Zhang, Wu, Hu, Yang, Gui, Liu, Wang, Liu, Lu, Xu, Leng, Li and Xu ^{3 ]}, which is a typical femtosecond high peak power laser. The nonlinear media for spectral broadening are fused silica TTPs, with the group delay dispersion (GDD) of approximately 36 fs²/mm and a nonlinear refractive index of approximately 2.5×10⁻⁷ cm²/GW at 800 nm central wavelength. The laser propagation in nonlinear media is simulated by a 3D nonlinear Schrödinger equation^[23], shown in Equation (1). Here, A is the envelope of electric field strength, z is the longitudinal coordinate, t is the time, β ₂ is the group velocity dispersion, ω ₀ and k ₀ are the central frequency and central wavenumber, respectively, and n ₀ and n ₂ are the linear and nonlinear refractive index, respectively. As the gain spectra of modulation instability (also known as SSSF)^[ Reference Bespalov and Talanov ^{24 ]} generally features a cutoff around hundreds of mm⁻¹, which corresponds to transverse uniformity of the beam profile with a typical size of a few micrometers, the resolution of our simulations is set as 2.5 μm. Besides, limited by computing power, a beam diameter of only 9 mm is adopted for numerical simulations and verifications. However, actually, the beam diameters of high peak power lasers are generally up to hundreds of millimeters:

(1) $$\begin{align}\frac{\partial A}{\partial z}=\frac{i}{2{k}_0}{\nabla}_{\perp}^2A+i{k}_0\frac{n_2}{n_0}{\left|A\right|}^2A-i\frac{\beta_2}{2}\frac{\partial^2A}{\partial {t}^2}-{k}_0\frac{n_2}{n_0{\omega}_0}\frac{\partial \left(A\cdot {\left|A\right|}^2\right)}{\partial t}.\end{align}$$

In the nonlinear propagation process, an arbitrary transverse wavevector K _⊥ (K ₀ = 2πn ₀ / λ ₀) propagates at an angle (θ = ±K _⊥ / K ₀) to the z-axis. In addition, the most serious characteristic angle is the direction in which the nonlinear process becomes phase matched, when considering the nonlinear contributions to the different characteristic angles. The most serious characteristic angle and corresponding spatial frequency can be calculated by Equation (2) ^[ Reference Khazanov, Mironov and Mourou ^{12 ]}:

(2) $$\begin{align}{\theta}_{{\max}}=\sqrt{\frac{2{n}_2I}{n_0}};{K}_{\perp {\max}}={K}_0{\theta}_{{\max}}=\frac{2\pi {n}_0}{\lambda_0}\sqrt{\frac{2{n}_2I}{n_0}}.\end{align}$$

For the 30 fs laser assumed above, the noise gain for different spatial frequency components is calculated, as shown in Figure 2(a) ^[ Reference Bliss, Hunt, Renard, Sommargwn and Weaver ^{25 ,} Reference Ginzburg, Kochetkov, Potemkin and Khazanov ^{26 ]}. The noise gain is calculated as the ratio of the noise fluences after and before the spectral broadening process. For simplicity, the spatial frequencies of all noises in the laser are set to ${K}_{\perp {\max}}$ (the calculated result is ~350 mm⁻¹) in the following spectral broadening process. On the one hand, the SSSF instability has the highest increment at this spatial frequency. Hence, if suppression at the peak of the instability gain, which shows the maximal SSSF suppression ability of this method, is satisfied, we may not need to be concerned about all the other ones. On the other hand, the noises at this frequency cannot be completely diffracted out by free propagation over a few meters in the compressors of ultrahigh peak power lasers, since their beam diameters generally reach up to hundreds of millimeters. Beam cleaning in a standard compressor is not the point of this work; hence we neglected temporal self-filtering in standard compressors^[ Reference Khazanov ^{27 ]}.

Figure 2 (a) The noise gain for different spatial frequency components. (b) The relationship between the achievable recompression pulse duration and the length of the fused silica TTPs.

To clearly show the physical nature of the AFGC in SSSF suppression, we used 30 fs pulses at each point of the beam cross-section and fluence distribution as a boundary condition for Equation (1) at z = 0. The attainable recompressed pulse durations of the 30 fs laser are also calculated based on the different lengths of the TTPs. As shown in Figure 2(b), sub-10 fs recompressed pulses can be achieved in the case of 1.0-mm-thick fused silica TTPs, which has also been experimentally proved in a similar femtosecond laser^[ Reference Kim, Kim, Yang, Yoon, Sung, Lee and Nam ^{15 ]}. Thereby, 1.0-mm-thick fused silica plates will be employed for spectral broadening in the following simulations, with a B-integral of approximately 5.5.

Figure 3(a) illustrates the spatial distribution of the initial 30 fs laser. The maximal beam fluence is 0.12 J/cm² and the PTA (peak-to-average) value of the beam fluence is 1.52. The left-hand and bottom curves correspond to the beam fluence on the central axis of the laser beam, and the same in the following figures. After passing through the 1.0-mm-thick fused silica TTPs, the fluence modulation becomes much more serious, and the maximal beam fluence greatly increases to 0.76 J/cm², shown as Figure 3(b). Such a large beam fluence will seriously destroy the following optical components and prevent the practical application of post-compression. To reveal more detail, the small areas in Figures 3(a) and 3(b) are zoomed in, as shown in Figures 3(c) and 3(d). It is obvious that serious SSSF occurs during the above spectral broadening process. Hence, the suppression of SSSF should be a core issue in the post-compression of high peak power lasers.

Figure 3 The spatial beam fluences of a 30 fs laser: (a) output from a standard compressor and (b) then after spectral broadening; (c), (d) zoomed-in of the corresponding areas in (a) and (b), respectively.

3 Post-compression after an asymmetric four-grating compressor

The novel post-compression scheme based on AFGC^[ Reference Shen, Du, Liang, Wang, Liu and Li ^{28 ]}, that is, L ₁ ≠ L ₂ in Figure 1, is proposed for high peak power lasers to overcome the challenge of SSSF. An AFGC can offer absolutely the same amount of temporal chirp for pulses compression as a standard compressor, as long as L ₂ + L ₁ are equal in both designs. Hence, the influence of residual temporal chirp on the following spectral broadening process can be ignored. By using the AFGC, a moderate spatial dispersion can be introduced to the output laser, which can effectively smooth the beam fluence^[ Reference Shen, Du, Liang, Wang, Liu and Li ^{28 ]}. The AFGC-induced spatial dispersion length can be written as in Equation (3), where ω _s and ω _l represent the shortest and the longest wavelength components of the input laser, respectively, and α and β are the incident and diffracted angles on G ₁, respectively. It is obvious that the spatial dispersion length d ₀ is proportional to the difference between L ₁ and L ₂. Because of the relatively strong diffraction ability of gratings, large spatial dispersion can be realized by a small L ₂ − L ₁:

(3) $$\begin{align}{d}_0=\left(\tan \beta \left({\omega}_{\mathrm{s}}\right)-\tan \beta \left({\omega}_{\mathrm{l}}\right)\right)\times \cos \alpha \times \left({L}_2-{L}_1\right).\end{align}$$

In order to demonstrate the advantages of the AFGC in SSSF suppression, a numerical simulation is also carried out based on the same 30 fs laser parameters as above. For the standard compressor above, the grating groove density is 1480 gr/mm, the grating pair separations are 1.0 m and the laser incident angle on G ₁ is $\alpha =$ 50°. These parameters are also referring to the compressor in our SULF-1 PW laser beamline^[ Reference Zhang, Wu, Hu, Yang, Gui, Liu, Wang, Liu, Lu, Xu, Leng, Li and Xu ^{3 ]}. To be an AFGC, two grating pair separations are altered, respectively, while keeping their sum constant (2 m). Figure 4(a) shows that the spatial dispersion length d ₀ is proportional to the difference between L ₁ and L ₂, while Figure 4(b) shows that the PTA drastically reduces with the increasing L ₂ − L ₁. The numerical simulation agrees well with the theoretical prediction (blue curve), which is deduced using Equations (8), (21), (27), (28) and (32) in Ref. [Reference Khazanov27]:

(4) $$\begin{align}\mathrm{PTA}_{\mathrm{out}}=\exp \left(-{\left(\frac{L_2-{L}_1}{l}\right)}^2\right)\left(\mathrm{PTA}_{\mathrm{in}}-\mathrm{PTA}_{\mathrm{ideal}}\right)+\mathrm{PTA}_{\mathrm{ideal}},\end{align}$$

Figure 4 (a) The spatial dispersion and (b) the PTA of beam fluence output from the AFGC, based on different L ₂ − L ₁ of the AFGC. (c) The noise gain curves of laser beams after the AFGC with different L ₂ − L ₁.

where:

(5) $$\begin{align}l=\frac{\omega_0{\tau}_{\mathrm{FWHM}}}{\sqrt{\mathit{\ln}2}\cdot {k}_{\perp {\max}}}\cdot \frac{\cos^3\beta \left({\omega}_0\right)}{\left(\sin \alpha +|\sin \beta \left({\omega}_0\right)|\right)\cos \alpha }.\end{align}$$

Here, $\mathrm{PTA}_{\mathrm{ideal}}=$ 1.16 is the result of an ideal 10th super-Gaussian beam without noise, and ω ₀ represents the central wavelength component of the input laser. The noise gain of the laser after the AFGC also reduces with the increase of L ₂ − L ₁, shown as Figure 4(c). In the case of L ₁ = 0.999705 m, L ₂ = 1.000295 m, the noise gain at 350 mm⁻¹ dramatically drops to 1.9, while it is 24 when a standard compressor is adopted. This difference L ₂ − L ₁ = 590 μm is very small compared with the initial grating pair separation of 1 m. Hence, the slight influence on the spatiotemporal quality of compressed pulses can be ignored^[ Reference Wang, Wang, Xu and Leng ^{29 ]}. Notably, the results in Refs. [Reference Khazanov27,Reference Shen, Du, Liang, Wang, Liu and Li28,Reference Du, Shen, Liang, Wang, Liu and Li30] have also proved that the temporal contrast and the focused peak intensity of compressed pulses output from an AFGC remain almost unchanged, compared with that of a standard compressor.

The beam fluence output from the above AFGC is shown in Figure 5(a). It is clear that the fluence modulation is greatly decreased, and the maximal beam fluence is reduced from initial 0.12 to 0.09 J/cm². Then, the smooth laser beam will also pass through the 1.0-mm-thick fused silica TTPs for spectral broadening. The output beam fluence is shown in Figure 5(b). As the noise gain is only 1.9, the maximal beam fluence is just increased to 0.09450 from 0.09446 J/cm². In addition, there is no evident degradation of the fluence modulation or the spatial uniformity in the above spectral broadening process. The small areas that correspond to Figure 3 are also zoomed in and are shown in Figures 5(c) and 5(d). Before and after the TTPs, there is no obvious difference in beam quality. The simulation results prove that the SSSF is effectively suppressed by the AFGC. Compared with Figure 3(b), the SSSF-induced fluence modulation and intensity spikes are overcome and a more uniform laser beam is achieved.

Figure 5 The spatial beam fluence of a 30 fs laser: (a) output from an AFGC and (b) then after the spectral broadening stage; (c), (d) zoomed-in of the corresponding areas in (a) and (b), respectively.

For the sake of simplicity, the spectral broadening and recompressing of the above smooth laser beam are char acterized by the simulated results based on the nonlinear Schrödinger equation, in which the laser intensity is approximated as the averaged intensity in the near-field. As a result, the spectral width is broadened from 60 nm to approximately 105 nm (FWHM), as shown in Figure 6(a). The asymmetry of the broadened spectrum is mainly induced by the self-steepening effect. Lastly, the residual dispersion of the spectral broadened laser is compensated by using broadband CMs. The additional GDD, introduced by the self-phase modulation (SPM) process and the nonlinear materials, is about 80 fs². After being reflected by two broadband CMs with a total GDD of –80 fs², sub-10 fs ultrashort laser pulses are expected, as shown in Figure 6(b).

Figure 6 (a) The spectra of laser pulses before and after spectral broadening. (b) The pulse durations before and after post-compression with an AFGC.

4 Post-compression at different initial noise intensities

For the initial laser beams with different noise intensities compared to Figure 3(a), the PTAs of the beam fluence after the spectral broadening process and the corresponding noise gain are also investigated, as shown with the upper two curves in Figures 7(a) and 7(b). Due to the saturation effect, the PTA growth of output beam fluence gradually flattens out and the noise gain rapidly reduces, with the increase of initial noise fluence. Physically, the saturation can be explained by the reduction of fluence transferring from the main laser to the noise. When the noise fluence is high enough to be compatible with the main laser fluence, the instability increment decreases. In other words, the noise gain rapidly increases with the reduction of initial noise intensity, that is, the PTA of the initial beam fluence. The noise gain can reach approximately 2.4×10⁴ when the initial PTA is 1.17. In this case, serious SSSF will occur in post-compression with a standard compressor, as shown in Figures 7(c) and 7(e), but a smooth laser beam still can be achieved by applying an AFGC (L ₂ − L ₁ = 590 μm, the same in all cases) before post-compression, as shown in Figures 7(d) and 7(f). Hence, an AFGC may be also indispensable for the post-compression of high peak power lasers, even if the laser beams before nonlinear media are good enough.

Figure 7 (a) The PTA of the beam fluence after spectral broadening with a 1-mm-thick TTP and (b) the corresponding noise gain, based on different initial laser beams. The beam fluences of lasers after spectral broadening with a 1-mm-thick TTP, with (c) a standard compressor and (d) an AFGC. (e), (f) Zoomed-in of the corresponding areas in (c) and (d), respectively.