SATPC0038046 Tab 07 SOW_Redacted.pdf

This document is a Statement of Work (SOW) for a Thin-Wall Turn Around Manifold Directed Energy Deposition Component for NASA's Marshall Space Flight Center. The SOW requires a vendor to fabricate and provide engineering support for a laser powder directed energy deposition (LP-DED) of an RS-25 aft nozzle turnaround manifold, with specific technical requirements including:

Key technical specifications include fabricating a 1 mm wall thickness component using JBK-75 Fe-Ni alloy, demonstrating LP-DED on a large-scale machine platform with a build height over 90", and completing a 55-consecutive day print period (approximately 1,000 hours). The vendor must provide comprehensive support including engineering assistance, machine operation, consumables, and tool code generation. The project has a 6-month performance period, with the primary deliverable being DED samples and reporting from the manifold build, to be shipped to Marshall Space Flight Center in Huntsville, Alabama.