Low temperature sensitivity coefficients of gun propellants are of great significance for improving the stability of weapon performances. In this work, RDX-NC-NG-DEGDN propellants (R-MNEGP) were prepared to reduce the temperature sensitivity coefficient of mixed charges. The temperature sensitivity coefficients of R-MNEGP, NC-NG-DEGDN propellants (MNEGP) and their mixed charges were studied by closed vessel tests, scanning electron microscope (SEM), and ballistic firing experiments. The results show that the increased burning surface of R-MNEGP compensates the decrease in the burning rate of the propellant when the initial temperature is decreased compared with MNEGP. The temperature sensitivity coefficient of R-MNEGP is lower than that of MNEGP, and the temperature sensitivity coefficients of the mixed charges (R-MNEGP and MNEGP) are between these two temperature sensitivity coefficients in the range of À 40°C-20°C and 20°C-50°C. Compared with MNEGP, the velocity temperature sensitivity coefficients of the mixed charges with 6 wt % and 10 wt % R-MNEGP decreased by 34.86 % and 70.67 %, and the pressure temperature sensitivity coefficients of these decreased by 42.99 % and 100.90 % with increasing temperature from À 40°C to 15°C. And the velocity temperature sensitivity coefficients had no significant change, and the pressure temperature sensitivity coefficients decreased by 2.58 % and 77.98 % in the range of 15°C-50°C. This study offers an attractive strategy for tuning the temperature sensitivity coefficient by mixing charges of R-MNEGP and MNEGP with different temperature sensitivity coefficients.