This paper develops a parametrically homogenized continuum damage mechanics (PHCDM) model for unidirectional fiber reinforced epoxy composites undergoing progressive damage. The PHCDM models are designed to overcome limitations of prohibitive computational overhead associated with many homogenization methods. They are thermodynamically consistent, reduced order continuum models with explicit representation of microstructural morphology through strategically determined parameters. The PHCDM model is derived from detailed micromechanics simulations of the representative volume element (RVE) using energy equivalence principles. Micromechanical failure is due to fiber–matrix interface debonding and matrix cracking. The macroscopic PHCDM models represent damage anisotropy through a second order damage tensor that contributes to the evolution of a damage surface in the space of damage work conjugate. The damage surface characterizes the initiation and evolution of damage in the composite. The constitutive relation between damage and its work conjugate is represented by an anisotropic fourth order damage surface tensor Pijkl, whose components are expressed as functions of current damage state. These are calibrated and validated from homogenized micromechanics (HMM) simulations. The PHCDM model is incorporated in a commercial finite element code and structural analysis of macroscopic composite components are executed for understanding concurrent damage and failure at multiple scales.