SATPC0040252 Tab 07 2 SOW Redacted.pdf

PDF 165 KB Posted Feb 5, 2026

Attached to: InRoDES Gas Generator Version 1 Machining
Solicitation number: 80NSSC26923334Q
Issued by: National Aeronautics and Space Administration Shared Services Center

About this file

Written by GovTribe AI · Feb 5, 2026

This is a Statement of Work (SOW) for precision machining and welding fabrication services for NASA's Marshall Space Flight Center (MSFC) in support of the InRoDES Gas Generator Version 1 project. The work spans from January 13, 2026 through June 1, 2026.

The SOW encompasses four tasks: Task 1 requires machining 12 injectors of various part numbers from additively manufactured ORCAlloy-21; Task 2 requires machining 8 chambers (three different part numbers) from additively manufactured GRX-810; Task 3 requires machining 4 converging throats, 4 sensor ports, and welding 4 converging throat assemblies from GRX-810; and Task 4 requires machining 4 elbow halves and welding 2 elbows from GRX-810. All work must comply with specified drawing specifications, with completion required within 10 working days of receiving each set of parts from NASA. The contractor must provide detailed ISO 9001:2015 inspection reports for all completed work and immediately notify NASA of any noncompliance, with NASA providing replacement parts at no additional cost if parts are deemed unacceptable.

The contractor must demonstrate specific qualifications including: ISO 9001:2015 certification, experience achieving 16 Ra surface finish on both ORCAlloy-21 and GRX-810 with documented examples or physical parts, dimensional tolerances of ±0.004" or better on both materials, and experience machining all AS5202 port types with AN fitting verification. Additionally, the contractor must have ITAR compliance capability and be responsible for providing all necessary fixturing, tooling, and support hardware. All completed parts and inspection reports shall be shipped to Central Receiving, Building 4631, Marshall Space Flight Center, Huntsville, AL 35812.

View the file

On GovTribe

Work with this file

Download the original file
Contacts named in this file
Similar government files
Ask GovTribe AI about this file

Try for free Login

Text version

The file's text, extracted by GovTribe without its formatting.

InRoDES Gas Generator Version 1 Machining Statement of Work (SOW)

January 13, 2026

The National Aeronautics and Space Administration (NASA), specifically Marshall Space Flight Center (MSFC), requires fabrication services for Gas Generator Version 1 hardware in support of the InRoDES project. These fabrication services include precision machining and welding of additively manufactured components.

Task 1, Machining of Injectors

1. The contractor shall machine a total of 12 injectors. The part numbers and quantities are as follows:

• MC331A03: Quantity 2

• MC331B03: Quantity 2

• MC331C03: Quantity 2

• MC331D03: Quantity 1

• MC331E03: Quantity 1

• MC331F03: Quantity 1

• MC331G03: Quantity 1

• MC331H03: Quantity 1

• MC331J03: Quantity 1

2. All parts shall be machined according to drawing specifications as provided in requirement 1.1. The contractor shall verify compliance with the specifications using their internal inspection processes or as approved by NASA MSFC engineering.

3. Upon completion of the inspection, the contractor shall provide NASA with a detailed inspection report per ISO 9001:2015.

4. If a part is found to be noncompliant with the drawing specifications, the contractor shall notify NASA immediately. Noncompliance is defined as failure to meet dimensional tolerances, omission of required steps outlined in the drawing notes or flag notes, or failure to adhere to any other explicit instructions specified in the drawing. NASA will evaluate the impact of the noncompliance. If the part is deemed unacceptable, NASA will provide a replacement part for machining at no additional cost to NASA.

5. The contractor shall complete all machining work no later than 10 working days from receipt of each set from NASA.

6. The contractor shall have demonstrated experience achieving a surface finish of 16 Ra on additively manufactured ORCAlloy-21. The contractor shall provide documented examples or physical parts they have previously machined from ORCAlloy-21 that meet this surface finish requirement.

7. The contractor shall have demonstrated experience achieving dimensional tolerances of ±0.004" or better on additively manufactured ORCAlloy-21.

8. The contractor shall have experience machining all AS5202 port types in additively manufactured ORCAlloy-21. The contractor shall verify the threads using the appropriate AN fitting to ensure compliance with specifications.

9. The contractor shall hold certification to ISO 9001:2015 quality management standards.

10. The contractor shall have the capability to handle ITAR-controlled data and parts, ensuring compliance with all applicable regulations.

11. The contractor shall be responsible for providing all necessary fixturing, tooling, and support hardware required to complete the machining of the parts.

Task 2, Machining of Chambers

1. The contractor shall machine a total of 8 chambers. The part numbers and quantities are as follows:

• MC331106-011: Quantity 3

• MC331105-011: Quantity 2

• MC331104-011: Quantity 3

2. All parts shall be machined according to drawing specifications as provided in requirement 2.1. The contractor shall verify compliance with the specifications using their internal inspection processes or as approved by NASA MSFC engineering.

3. Upon completion of the inspection, the contractor shall provide NASA with a detailed inspection report per ISO 9001:2015.

5. The contractor shall complete all machining work no later than 10 working days from receipt of each set from NASA.

6. The contractor shall have demonstrated experience achieving a surface finish of 16 Ra on additively manufactured GRX-810. The contractor shall provide documented examples or physical parts they have previously machined from GRX-810 that meet this surface finish requirement.

7. The contractor shall have demonstrated experience achieving dimensional tolerances of ±0.004" or better on additively manufactured GRX-810.

8. The contractor shall have experience machining all AS5202 port types in additively manufactured GRX-810. The contractor shall verify the threads using the appropriate AN fitting to ensure compliance with specifications.

9. The contractor shall hold certification to ISO 9001:2015 quality management standards.

10. The contractor shall have the capability to handle ITAR-controlled data and parts, ensuring compliance with all applicable regulations.

11. The contractor shall be responsible for providing all necessary fixturing, tooling, and support hardware required to complete the machining of the parts.

Task 3, Machining and Welding of Converging Throats

1. The contractor shall machine a total of 4 converging throats. The part numbers and quantities are as follows:

• MC331202-033: Quantity 4

2. The contractor shall machine a total of 4 sensor ports. The part numbers and quantities are as follows:

• MC331203-001: Quantity 4

3. The contractor shall weld a total of 4 converging throat assemblies. The part numbers and quantities are as follows:

• MC331202-011: Quantity 4

4. All parts shall be machined and welded according to drawing specifications as provided in requirement 3.1 – 3.3. The contractor shall verify compliance with the specifications using their internal inspection processes or as approved by NASA MSFC engineering.

5. Upon completion of the inspection, the contractor shall provide NASA with a detailed inspection report per ISO 9001:2015.

6. If a part is found to be noncompliant with the drawing specifications, the contractor shall notify NASA immediately. Noncompliance is defined as failure to meet dimensional tolerances, omission of required steps outlined in the drawing notes or flag notes, or failure to adhere to any other explicit instructions specified in the drawing. NASA will evaluate the impact of the noncompliance. If the part is deemed unacceptable, NASA will provide a replacement part for machining at no additional cost to NASA.

7. The contractor shall hold certification to ISO 9001:2015 quality management standards.

8. The contractor shall have the capability to handle ITAR-controlled data and parts, ensuring compliance with all applicable regulations.

9. The contractor shall be responsible for providing all necessary fixturing, tooling, and support hardware required to complete the machining and welding of the parts.

Task 4, Machining and Welding of Elbows

1. The contractor shall machine a total of 4 elbow halves. The part numbers and quantities are as follows:

• MC331304: Quantity 2

• MC331305: Quantity 2

2. The contractor shall weld a total of 2 elbows. The part numbers and quantities are as follows:

• MC331303-001: Quantity 2

3. All parts shall be machined and welded according to drawing specifications as provided in requirement 4.1 – 4.2. The contractor shall verify compliance with the specifications using their internal inspection processes or as approved by NASA MSFC engineering.

4. Upon completion of the inspection, the contractor shall provide NASA with a detailed inspection report per ISO 9001:2015.

5. If a part is found to be noncompliant with the drawing specifications, the contractor shall notify NASA immediately. Noncompliance is defined as failure to meet dimensional tolerances, omission of required steps outlined in the drawing notes or flag notes, or failure to adhere to any other explicit instructions specified in the drawing. NASA will evaluate the impact of the noncompliance. If the part is deemed unacceptable, NASA will provide a replacement part for machining at no additional cost to NASA.

6. The contractor shall complete all machining work no later than 10 working days from receipt of each set from NASA.

7. The contractor shall have demonstrated experience achieving a surface finish of 16 Ra on additively manufactured GRX-810. The contractor shall provide documented examples or physical parts they have previously machined from GRX-810 that meet this surface finish requirement.

8. The contractor shall have demonstrated experience achieving dimensional tolerances of ±0.004" or better on additively manufactured GRX-810.

9. The contractor shall have experience machining all AS5202 port types in additively manufactured GRX-810. The contractor shall verify the threads using the appropriate AN fitting to ensure compliance with specifications.

10. The contractor shall hold certification to ISO 9001:2015 quality management standards.

11. The contractor shall have the capability to handle ITAR-controlled data and parts, ensuring compliance with all applicable regulations.

12. The contractor shall be responsible for providing all necessary fixturing, tooling, and support hardware required to complete the machining of the parts.

Period of Performance (POP) January 13, 2026 through June 1, 2026

Shipping

1. Contractor shall ship all deliverables to:

Central Receiving, Bldg 4631

Marshall Space Flight Center Huntsville, AL 35812

Deliverables

1. Completed parts machined under Task 1, along with detailed inspection reports demonstrating compliance with Task 1 specifications.

2. Completed parts machined under Task 2, along with detailed inspection reports demonstrating compliance with Task 2 specifications.

3. Completed parts machined and welded under Task 3, along with detailed inspection reports demonstrating compliance with Task 3 specifications.

4. Completed parts machined and welded under Task 4, along with detailed inspection reports demonstrating compliance with Task 4 specifications.

File details come from the government source that posted it. Updated Feb 5, 2026.