In this paper, we propose models and methods for the simulation of two-phase flows in Liquid Rocket Engines (LRE) under subcritical conditions. The numerical strategy consists into coupling models dedicated to different topologies. Actually, we propose a five equation diffuse interface model for the treatment of the dense "separated two-phase flow" near the injector and an Eulerian kinetic based model for the "dispersed two-phase flow" in the chamber. We derive a novel formulation of the 5 equation system to build a robust HLLC type scheme. Then we use a fully Eulerian coupling strategy to take into account for primary atomization. We first run classical test cases in order to validate the numerical methods. Then a simulation on a test case representative to one coaxial injector is performed under subcritical conditions.