Additive Manufacturing of Inconel 718 Turbine Components via SLM Solutions 280

The contract requires the performance of laser powder bed fusion additive manufacturing using the SLM Solutions 280 machine to produce turbine blades and shaft assemblies from Inconel 718, a high-performance nickel-based superalloy specified for its strength and thermal resistance under extreme conditions. The manufacturing process must adhere strictly to NASA-MSFC drawing MC34120-003 and the associated manufacturing plan 34120-MFG-PLAN, ensuring dimensional accuracy, material integrity, and mechanical properties aligned with NASA’s mission-critical standards. A design of experiments (DOE) component is included to systematically optimize laser parameters such as power, scan speed, hatch spacing, and layer thickness to achieve defect-free, high-density parts with consistent microstructure and mechanical performance. All work must be completed in compliance with federal procurement standards and delivered by the response deadline of August 4, 2026. The solicitation is classified as a subcontract under NAICS code 333314, indicating it pertains to the manufacturing of industrial machinery, and is managed by the NASA Shared Services Center on behalf of the National Aeronautics and Space Administration. While no specific place of performance or point of contact is provided, the nature of the work implies the need for a qualified additive manufacturing facility with demonstrated capability in aerospace-grade metal AM, experience with Inconel 718, and familiarity with NASA-specific technical documentation and quality assurance protocols.