SATPC0037411 Tab 04 4 SOW_Redacted.pdf
PDF 2 MB Posted
- Attached to
- Additive Manufacturing Material Characterization and Data Dissemination Federal contract opportunity
- Solicitation number
- 80NSSC25893400Q
About this file
This Statement of Work (SOW) outlines NASA Space Technology Mission Directorate's requirements for additive manufacturing material characterization and data dissemination in partnership with Auburn University. The work involves characterizing AM alloy samples previously tested under RAMPT, completing detailed analysis of mechanical test data, and conducting extensive material characterization including scanning electron microscopy, computer tomography scanning, and optical microscopy.
The contractor must analyze 31 different materials including various Haynes alloys, Inconel variants, titanium alloys, and the GRX-810 alloy, documenting tensile and fatigue behaviors at different temperatures and conditions. Key deliverables include data summary sheets for all materials tested, draft or published technical reports for each material, and participation in bi-monthly progress meetings. The period of performance is 9 months from authority to proceed, with deliverables to be shipped to Marshall Space Flight Center in Huntsville, AL. The project requires a minimum 25% cost share from the contractor for aspects like machine development, materials, labor, and testing.
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Other files for this federal contract opportunity
| File | Type | Posted |
|---|---|---|
| SATPC0037411 Tab 07 Capability Statement Non-Commercial.pdf |
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Text version
24 6061-RAM2
Tensile/Fatigue behaviors of LP-DED A6061-RAM2: Effects of powder reuse and part orientation
25 Ti6242 Heat Treatment and Tensile and fatigue behavior of LP-DED Ti6242 at room and elevated temps
26 GRX-810
Fatigue Properties of Additively Manufactured GRX-810 Alloy at Room
Temperature: Effect of Post-Processing {HCF)
27 GRX-810
Fatigue Properties of Additively Manufactured GRX-810 Alloy at Elevated
Temperatures: Effect of Post-Processing {HCF)
28 GRX-810
Tensile Properties of Additively Manufactured GRX-810 Alloy at Room and
Elevated Temperatures
29 GRX-810
Low Cycle Fatigue Behavior of Additively Manufactured GRX-810 Alloy :
Effect of Post-Processing and Test Temperature
30 GRX-810
Effect of Build Orientation on Tensile and Fatigue properties of Additively
Manufactured GRX-810 Alloy
31 AISxl Effect of HIP and heat treatment of tensile/fatigue at various temperatures of AISXl
Shipping
1. Contractor shall ship any deliverables as needed to:
Marshall Space Flight Center
Central Receiving, Bldg 4631
Huntsville, AL 35812
Period of Performance {POP)
• 9 months from authority to proceed (ATP)
Deliverables
1. Data summary sheets related to tensile and fatigue properties for each of the alloys provided in table 1.
2. A draft or published report for each material outlined in Table 1.
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