SATPC0040561 Tab 04 4 SOW..pdf

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Attached to
Aheadd CP-1 NXG Build Federal contract opportunity
Solicitation number
80NSSC26927313Q
Issued by
National Aeronautics and Space Administration Shared Services Center

About this file

This is a Statement of Work (SOW) for NASA's Marshall Space Flight Center (MSFC) requiring the manufacturing of Aheadd CP-1 material testing and characterization specimens using a Nikon SLM Solutions NXG additive manufacturing machine. The primary objective is to evaluate the viability of this platform for cryogenic fluid management (CFM) components and characterize material produced on large-scale laser powder bed fusion machines. The vendor must have prior experience manufacturing Aheadd CP-1 with laser powder bed fusion (L-PBF) technology and shall develop a build layout using best practices in coordination with NASA before manufacturing begins. The vendor is responsible for processing provided build files to achieve the highest feasible resolution, printing labels on all specimens with build and specimen numbers, de-powdering specimens, and removing them from the build plate using wire EDM or bandsaw in the as-built condition.

The specimen matrix comprises 207 total printed parts across multiple categories: 43 tensile specimens (40 vertical, 18 horizontal stacked), 45 high-cycle fatigue (HCF) specimens (30 vertical prepolish, 12 vertical as-built, 18 horizontal stacked), 48 low-cycle fatigue (LCF) specimens, 20 blank cylinders for metallography and thermophysical testing, 8 grouped thin section specimens, 12 laser quality parts, 4 challenge parts (2 lattice boxes with shroud and 2 without), 2 powder cups, 4 cryo coefficient of thermal expansion (CTE) rectangular blocks, and 6 fatigue crack growth blocks. Deliverables include printed specimens per the agreed specimen matrix and documentation on build pedigree, including powder certificates of conformance with material composition and laser assignment parameters. All specimens shall be shipped to Marshall Space Flight Center Central Receiving in Huntsville, Alabama 35812. The period of performance is ten (10) weeks from contract award.

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SATPC0040561 Tab 06 RDSS..pdf PDF
SATPC0040561 Tab 07 Capability Statement.pdf PDF

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Aheadd CP-1 NXG Specimen Build

Statement of Work (SOW)

The National Aeronautics and Space Administration (NASA), specifically Marshall Space Flight Center (MSFC) has a need for manufacturing of Aheadd CP-1 material testing and characterization specimens using a Nikon SLM Solutions NXG additive manufacturing machine to evaluate the viability of using this platform for cryogenic fluid management (CFM) components and to better characterize material produced on large scale laser powder bed fusion machines.

The SOW is as follows:

1. The vendor shall have experience manufacturing Aheadd CP-1 with laser powder bed fusion (L-PBF) additive manufacturing.

2. The vendor shall develop a build layout using vendor’s best practices, the specimen matrix, and build files or geometries provided by NASA, and review with NASA prior to manufacturing.

3. The provided build files shall be processed by the vendor using best practices to ensure the highest resolution feasible for the specimens and that sufficient stock material is added to account for build plate removal.

4. The vendor shall print labels on all specimens notating the build and specimen number.

5. The vendor shall de-powder the specimens and remove from the build plate using wire

EDM or bandsaw in the as-built condition.

6. NASA will provide detailed specimen matrix, specimen files, and discuss as necessary.

Specimen Matrix

Part Name Contents

QTY/Type Total Printed

Parts File/Geometry

Tensile Specimens

40 Vertical

Tensile_ASTM_E8_Short 18 Horizontal (3 stacks of 6) Stacked TN_1

HCF

30 Vertical

HCF Prepolish 12 Vertical As-

Built HCF As-Built

18 Horizontal (3 stacks of 6)

Stacked TN_1

LCF 48 Vertical 48 LCF Polish Metallography and

Thermophysical 20 Blank Cylinders 20 0.6”diameter 4” tall

Thin sections 8 grouped specimens 8 Thin Section with Stock

Laser Quality 12 12 Nikon recommended geometry

Challenge Parts Small geometric parts. 4

2 lattice boxes with shroud

2 lattice boxes without a shroud

Powder Cups 2 2 Nikon recommended geometry

Cryo CTE 4 Rectangular Blocks 4 1.25”x0.6”x4” block

Fatigue Crack Growth 6 Blocks 6 3”x0.75”x3”

Shipping

1. Contractor shall ship all deliverables and returned samples to:

Marshall Space Flight Center Central Receiving, Huntsville, AL 35812

Deliverables

1. Printed Aheadd CP-1 specimens per the specimen matrix provided and agreed upon.

2. Documentation on the build pedigree including but not limited to:

a. Powder certificate of conformance with material composition for powder lots used

b. Laser assignment and parameters that may be included in a standard job report.

Period of Performance

The tasks shall be performed within ten (10) weeks of contract award.

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