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Additive Manufacture of Refractory Alloy C103 for Propulsion ApplicationsC103 is niobium alloy used in high temperature operating environments. Traditional manufacture methods suffer from feedstock constraints, difficult to machine, high buy-to-fly ratios, and high costs resulting in a limited number of suppliers. Additive manufacture (AM) offers advantages in production of complex parts, improved properties, reproducibility, with significant material cost and schedule savings. The objectives of this project was to investigate the feasibility to AM C103, develop powder feedstock, optimize process parameters, establish design criteria, investigate post-process heat treatments, and determine material properties. AM C103 proved feasible, increased design flexibility, improved mechanical properties compared to wrought, and resulted in an order of magnitude cost reduction.
Document ID
20205003674
Acquisition Source
Marshall Space Flight Center
Document Type
Abstract
Authors
Omar R Mireles
(Marshall Space Flight Center Redstone Arsenal, Alabama, United States)
Omar L Rodriguez
(Sikorsky Aircraft Corporation (United States) Huntsville, Alabama, United States)
Youping Gao
(Castheon Inc Thousand Oaks, California, United States)
Noah Philips
(Allegheny Technologies (United States) Pittsburgh, Pennsylvania, United States)
Date Acquired
June 18, 2020
Publication Date
September 14, 2020
Publication Information
Subject Category
Composite Materials
Meeting Information
Meeting: JANNAF Liquid Propulsion Subcommittee (LPS) Advanced Materials Panel (AMP) Additive Manufacturing for Propulsion Applications Technical Interchange Meeting
Location: Virtual
Country: US
Start Date: September 14, 2020
End Date: September 18, 2020
Sponsors: Joint Army-Navy-NASA-Air Force (JANNAF)
Funding Number(s)
CONTRACT_GRANT: 80MSFC18N0001
Distribution Limits
Public
Copyright
Public Use Permitted.
Technical Review
NASA Peer Committee

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