At present, CNES has developed two aerothermodynamics tools named DEBRISK and PAMPERO, in order to assess the ground risk of debris. This paper will be focused on PAMPERO, a new tool based on a spacecraft-oriented approach. This code calculates the entire trajectory of one object by 6 DOF simulations, coupled with a 3D thermal module and ablation. The different modules will be presented. Comparisons and validations have been performed. Elaboration of a new spacecraft-oriented tool: PAMPERO

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