This document summarizes a critical design review for a project to develop an additive manufacturing system for printing solid rocket propellant. It outlines the project background, functional requirements, critical elements, and safety considerations. Key aspects of the design include the laser system selection, thermal modeling of the sintering process, powder bed subsystem, and implementation of safety systems to address the fire and explosion risks of the propellant materials. The goal is to 3D print complex grain shapes for solid rocket motors and compare the mechanical properties to those of traditionally cast propellant.