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This Zenodo project contains all the data used or obtained from the paper: X. Wang and T. Lafleur, “Global modelling and performance analysis of a water-fueled radio-frequency gridded ion thruster,” Journal of Applied Physics (2026). https://doi.org/10.1063/5.0312768 The reaction rate coefficient data can be found in: H2O_Rate_Coefficients.xlsx H2_Rate_Coefficients.xlsx O2_Rate_Coefficients.xlsx OH_Rate_Coefficient.xlsx H_Rate_Coefficients.xlsx O_Rate_Coefficients.xlsx The thermal conductivity of xenon can be found in: Xenon thermal conductivity.dat The corresponding figures for the uploaded data are listed below: Figure 2a, 2b - RF power based densities.xlsx Figure 2c - RF power based neutral temperature.xlsx Figure 2d - RF power based electron temperature.xlsx Figure 3a - RF power based neutral composition ratio.xlsx Figure 3b - RF power based ion composition ratio.xlsx Figure 4a, 4b- Mass based densities.xlsx Figure 4c - Mass based neutral temperature.xlsx Figure 4d - Mass based electron temperature.xlsx Figure 5a - Mass based neutral composition ratio.xlsx Figure 5b - Mass based ion composition ratio.xlsx Figure 6a - RF power based thrust.xlsx Figure 6b - Mass based thrust.xlsx Figure 7a, 7b - RF power based efficiencies.xlsx Figure 8 - Mass based efficiencies.xlsx Figure 9a - RF power based Isp.xlsx Figure 9b - Mass based Isp.xlsx Figure 11a (simulated ion beam current)- RF power based ion beam current.xlsx Figure 11b (simulated ion beam current)- Mass based ion beam current 1.14W.xlsx, Mass based ion beam current 1.72W.xlsx, Mass based ion beam current 2.55W.xlsx, Mass based ion beam current 5.06W.xlsx, Mass based ion beam current 6.60W.xlsx Note: For the thrust, the uploaded data are in units of newtons (N) rather than millinewtons (mN), and the species composition ratios are given as fractions rather than percentages. In the paper, the thrust values were converted to mN, and the species composition ratios were converted to percentages.