Abstract: When high-velocity fragment impacted the fuel tank, hydrodynamic ram occurred. The fuel spurt caused by hydrodynamic ram may result in the ignition or even explore of the fuel tank, thus threatening the survivability of the high-value target. To study the characteristics of fuel spurt caused by the hydrodynamic ram event, the experiment of high-velocity fragment impacting the simulated fuel tank was conducted, and the characteristics of velocity and spatial distribution of the fuel spurt were tested and analyzed. In order to quantitatively described the initial motion velocity of the fuel spurt and the attenuation process of its movement in the air, the specific volume unit within the fuel was defined as fuel mass. The concepts of initial motion velocity and dispersion velocity of the fuel mass were proposed. And the process of fuel mass spurting from the penetration orifices was simplified into three stages: a) the fuel mass was about to spurt out, b) the fuel mass spurted from the penetration orifices; c) the fuel mass was moving in the air and gradually become atomized. On this basis, the theoretical model of the distribution of fuel spurt was established. According to the cracks at the penetration orifices and the shape change of the material at the edge of the orifices, the value of the coefficient of discharge were classified, and the influence of the distribution of pressure in the fuel was also taken into account during the calculation. When u0 ≤ 737 m/s, the range of Cv is from 0.60 to 0.70. When 737 m/s < u0 < 906 m/s, Cv ranges from 0.25 to 0.55. When u0 ≥ 906 m/s, Cv ranges from 0.75 to 0.95. The research showed that the average error between the calculation results of the fuel spurt axial distance and the experimental results was less than 15%. The error between the calculation results of the corrected theoretical model of radial distance and the experimental results was about 5%. The calculated results of the theoretical model were in good agreement with the experimental results.