Earth penetration weapon (EPW) is applicable for attacking underground targets protected by reinforced concrete and rocks. With increasing impact velocity, the mass loss/abrasion of penetrator increases, which significantly decreases the penetration efficiency due to the change of nose shape. The abrasion may induce instability of the penetrator, and lead to failure of its structure. A common disadvantage, i.e. dependence on corresponding experimental results, exists in all the available formulae, which limits their ranges of application in estimating the mass loss of penetrator. In this paper, we conduct a parametric study on the mass loss of penetrator, and indicate that the mass loss of penetrator can be determined by seven variables, i.e., the initial impact velocity, initial nose shape, melting heat, shank diameter of projectile and density and strength of target as well as the aggregate hardness of target. Further discussion on factors dominant in the mass abrasion of penetrator are given, which may be helpful for optimizing the target or the projectile for defensive or offensive objectives, respectively.Keywords Penetrator · Mass loss · Depth of penetration · Parametric study
List of symbolsA surface area of projectile nose (m 2 ) b length of projectile nose (m) C proportional coefficient of mass loss to initial kinetic energy of projectile (s 2 m −2 ) C p specific heat at constant pressure (J (kg K) −1 ) d shank diameter of projectile (m) f friction force per unit area (Pa) f c unconstrained compressive strength of concrete target (Pa) F n instant axial drag force on projectile nose (N) H Moh's hardness of aggregate H 0 reference value of Moh's hardness of aggregate k mechanical equivalent of heat (J cal −1 ) m instant mass of projectile (kg) M 0 initial mass of projectile (kg) M f mass of residual projectile (kg) N * instant nose factor of projectile N * 0 initial nose factor of projectile N * 1 and N * 2 dimensionless constant related to nose geometry p pressure on projectile nose (Pa) Q melting heat for unit mass of projectile (cal) R c Rockwell hardness S empirical constant for concrete target and related to f c t time (s) T Kelvin temperature (K) v instant penetration velocity (m s −1 ) 123 586 L. He et al. V s initial impact velocity of projectile (m s −1 ) w t friction work (J) z instant DOP of projectile (m) Z ultimate DOP of projectile (m) χ constant defined in Ref. [23] (kg m −3 )