The Department of Defense (DOD) is seeking proposals for the development of high power and torque electric motors for direct-drive rotorcraft applications. The objective is to identify and design an electric motor architecture that can provide high power and torque output at low rotational speeds suitable for rotorcraft applications. The proposed motor should be capable of delivering power in the range of 400-700+ horsepower at rotational speeds of 250-400 RPM, with torque ranging from 5,000-15,000+ ft-lb. The motor should also exhibit high torque densities in both continuous and short-term hover operations. The development of such motors is crucial for the advancement of electric aviation and would have immediate applications in light rotary-wing designs, eVTOL unmanned aircraft systems (UAS), and logistics operations. The project will involve a phased approach, starting with a feasibility analysis and conceptual design in Phase I, followed by detailed design and prototype development in Phase II. Phase III will focus on the integration and testing of the motor in a relevant aerospace application. The project duration is not specified, but the solicitation is open until March 31, 2025. For more information, visit the DOD SBIR 24.4 Annual solicitation notice on grants.gov or the DOD SBIR/STTR Opportunities website.