The document outlines the Statement of Work for a project focused on developing high-temperature resistant materials for rotating detonation rocket engines (RDREs) intended for the U.S. Space Force. RDREs operate using detonation-based combustion, offering higher efficiency and smaller combustor sizes compared to traditional engines. The project emphasizes the need for materials capable of enduring extreme conditions—temperatures ranging from 1600-3500K and pressures from 1.9-17.6 bar—without active cooling. Key requirements include the production of three ceramic composite panels designed for mechanical and oxidative testing, as well as four inner-body components subject to pre- and post-test analyses by the Air Force Research Laboratory (AFRL). The contractor must employ scalable manufacturing techniques and demonstrate prior success in similar testing environments to ensure material viability. The overall aim is to provide materials that can sustain the RDRE environment, enabling the U.S. Department of the Air Force and Space Force to leverage this advanced propulsion technology effectively. This document aligns with the objectives of government RFPs by emphasizing rigorous testing and material innovation critical to national defense aerospace advancements.