SUMMARYThis paper presents the second part of a work that aims at developing a mechanical model for the behaviour of propellant-like materials under high con"ning pressure and strain rate. The model is to be employed to determine the temperature rise due to mechanical dissipation during a dynamic penetration event. Using the kinematical and thermodynamic background derived in the "rst part, a viscoelastic}viscoplastic}compac-tion model is put forward and identi"ed. Viscoelasticity and compaction refer to the elastomeric nature of the material, while viscoplasticity, including implicit damage through dilatancy, re#ects its granular nature. Some numerical exercises are performed, in view of determining the major model forces and weaknesses, and of assessing the numerical algorithm robustness. A penetration event is preliminarily simulated, and a temperature rise "eld predicted. Necessary model improvements are "nally discussed, together with several ways of research for a longer term approach.