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This Government Contract opportunity from National Aeronautics And Space Administration was posted on May 12, 2026. The submission period has ended. Browse the details below for market research, or find similar active opportunities.

Mechanical & Microstructural Testing of Additively Manufactured Components

Closed
Federal

Contract Overview

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The contract involves performing comprehensive mechanical and microstructural testing on additively manufactured oxide dispersion strengthened (ODS) alloy components. The work includes tensile, creep, fatigue, and microstructural analyses such as scanning electron microscopy (SEM), energy-dispersive X-ray spectroscopy (EDS), and density measurements to ensure that the printed components achieve a density of at least 99.9% and meet strict high-temperature performance standards. Issued by the NASA Shared Services Center under the National Aeronautics and Space Administration, this subcontract falls under the NAICS code 541380. It requires timely submission of responses by May 15, 2026, and focuses on validating the structural integrity and quality of advanced 3D-printed aerospace materials, critical for NASA's high-performance applications.

General Info

Perform mechanical and microstructural testing on ODS alloy components ensuring 99.9% density.

Agency

National Aeronautics And Space Administration → NASA Shared Services Center

NAICS

541380 - Testing Laboratories and ServicesView NAICS

Place of Performance

MS, USA

Set-Aside

NONE

Documents

(0)

No documents available

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Timeline

PhaseClosed
Posted

subcontract

Response Deadline

Deadline has passed

Submission Closed

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Organization & Contact Information

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AgencyNational Aeronautics And Space Administration → NASA Shared Services Center
ContactsNo contacts available
OfficeN/A
Organization / Agency
National Aeronautics And Space Administration → NASA Shared Services Center
Office AddressN/A
ContactsNo contact information available

Full Description

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Perform tensile, creep, fatigue, and microstructural analysis (SEM, EDS, density) to validate printed ODS alloy components meet ≥99.9% density and high-temperature performance requirements.