Effects of grain size and temperature of double base solid propellants on internal ballistics performance

A conventional bullet or projectile driven by solid fuels accelerates in the barrel and reaches certain muzzle velocity, spin and propulsion energies. Combustion characteristics of solid fuels are the most important factor affecting bullet performance and maximum range. In this work, double base solid propellants of spherical geometry within the ranges of 300-425, 425-500, 500-600, 600-710 and 710-850 mu m in diameter and temperatures of -60, -40, -20, 0, 20, 40 and 60 degrees C, were investigated in terms of the effects of grain size and temperature on burn rate, internal barrel pressure and bullet velocity. Solid fuel properties such as fuel heat of combustion, density, combustion temperature, particle size and mass were measured. In a constant volume chamber, burn rate was measured for each fuel sample at different pressure and temperature. In addition, cartridges of 7.62 mmin diameter were made using sample solid fuels, and shooting tests were carried out with a special test barrel. In the tests, strains along the barrel were determined using strain gauges and the muzzle exit velocity of the bullet was measured with a doppler radar for calibrations. It was seen that the increase of fuel temperature and decrease of particle size increased burn rate, internal barrel pressure and bullet velocity. (C) 2015 Elsevier Ltd. All rights reserved.