• High Power Laser Science and Engineering
  • Vol. 13, Issue 2, 02000e13 (2025)
Linjun Li1,2, Zhantao Lu1,2, Xinglong Xie1,2,*, Meizhi Sun1..., Xiao Liang1, Qingwei Yang1, Ailin Guo1, Ping Zhu1, Xuejie Zhang1, Dongjun Zhang1, Hao Xue1,2, Guoli Zhang1,2, Rashid Ul Haq1,2, Haidong Zhu1, Jun Kang1 and Jianqiang Zhu1,2,*|Show fewer author(s)
Author Affiliations
  • 1National Laboratory on High Power Laser and Physics, Shanghai Institute of Optics and Fine Mechanics, Chinese Academy of Sciences, Shanghai, China
  • 2Center of Materials Science and Optoelectronics Engineering, University of Chinese Academy of Sciences, Beijing, China
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    DOI: 10.1017/hpl.2025.4 Cite this Article Set citation alerts
    Linjun Li, Zhantao Lu, Xinglong Xie, Meizhi Sun, Xiao Liang, Qingwei Yang, Ailin Guo, Ping Zhu, Xuejie Zhang, Dongjun Zhang, Hao Xue, Guoli Zhang, Rashid Ul Haq, Haidong Zhu, Jun Kang, Jianqiang Zhu, "Ultrafast characterization of plasma critical surface evolution in inertial confinement fusion experiments with chirped laser pulses," High Power Laser Sci. Eng. 13, 02000e13 (2025) Copy Citation Text show less
    A femtosecond laser pulse with a center wavelength of 808 nm and a pulse duration of 30 fs is coupled into a pulse stretcher. The pulse stretcher introduces group velocity dispersion, which stretches temporally the pulse duration by frequency–time chirp. This results in the generation of a chirped probe pulse with a duration of 1.7 ns and a spectral range of 780–860 nm. The time-dependent wavelength distribution of this stretched probe pulse allows for time-resolved probing of the evolving plasma dynamics under investigation.
    Fig. 1. A femtosecond laser pulse with a center wavelength of 808 nm and a pulse duration of 30 fs is coupled into a pulse stretcher. The pulse stretcher introduces group velocity dispersion, which stretches temporally the pulse duration by frequency–time chirp. This results in the generation of a chirped probe pulse with a duration of 1.7 ns and a spectral range of 780–860 nm. The time-dependent wavelength distribution of this stretched probe pulse allows for time-resolved probing of the evolving plasma dynamics under investigation.
    The experimental setup consists of the following optical components: M1–M7 are reflective mirrors, BS1 and BS2 are beam splitters, L1 and L2 are focusing lenses, G1 and G2 are gold-coated diffraction gratings and P is an aperture plate. Notably, M1, M2 and the target are all situated within a vacuum target chamber.
    Fig. 2. The experimental setup consists of the following optical components: M1–M7 are reflective mirrors, BS1 and BS2 are beam splitters, L1 and L2 are focusing lenses, G1 and G2 are gold-coated diffraction gratings and P is an aperture plate. Notably, M1, M2 and the target are all situated within a vacuum target chamber.
    The initial conditions for the simulation.
    Fig. 3. The initial conditions for the simulation.
    Measured probe beam spectrum (red line) and calculated spectrum (blue line). Without considering the change in the critical surface morphology, the probe beam is delayed relative to the drive beam by (a) 250 ps, (c) 940 ps and (e) 1035 ps. Considering the change in the critical surface morphology, the probe beam is delayed relative to the drive beam by (b) 250 ps, (d) 940 ps and (f) 1035 ps.
    Fig. 4. Measured probe beam spectrum (red line) and calculated spectrum (blue line). Without considering the change in the critical surface morphology, the probe beam is delayed relative to the drive beam by (a) 250 ps, (c) 940 ps and (e) 1035 ps. Considering the change in the critical surface morphology, the probe beam is delayed relative to the drive beam by (b) 250 ps, (d) 940 ps and (f) 1035 ps.
    The image on the CCD sensor (a) without the driving laser and (b) with the driving laser. Specifically, the zero-point in the figure represents the moment when the probe beam begins to interact with the target.
    Fig. 5. The image on the CCD sensor (a) without the driving laser and (b) with the driving laser. Specifically, the zero-point in the figure represents the moment when the probe beam begins to interact with the target.
    (a) Autocorrelation signals at different time delays (0, 200, 400, 600, 800 ps). (b) Critical surface expansion velocity measured from the autocorrelation signals (red line) and obtained from numerical simulations (blue line). (c) Critical surface position as a function of time measured from the autocorrelation signals (red line) and obtained from numerical simulations (blue line). (The negative sign in Figures 6(b) and 6(c) indicates that the direction of the plasma critical surface movement is opposite to the direction of the drive laser.)
    Fig. 6. (a) Autocorrelation signals at different time delays (0, 200, 400, 600, 800 ps). (b) Critical surface expansion velocity measured from the autocorrelation signals (red line) and obtained from numerical simulations (blue line). (c) Critical surface position as a function of time measured from the autocorrelation signals (red line) and obtained from numerical simulations (blue line). (The negative sign in Figures 6(b) and 6(c) indicates that the direction of the plasma critical surface movement is opposite to the direction of the drive laser.)
    Linjun Li, Zhantao Lu, Xinglong Xie, Meizhi Sun, Xiao Liang, Qingwei Yang, Ailin Guo, Ping Zhu, Xuejie Zhang, Dongjun Zhang, Hao Xue, Guoli Zhang, Rashid Ul Haq, Haidong Zhu, Jun Kang, Jianqiang Zhu, "Ultrafast characterization of plasma critical surface evolution in inertial confinement fusion experiments with chirped laser pulses," High Power Laser Sci. Eng. 13, 02000e13 (2025)
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