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Large Scale and Multi-Alloy Rocket Engine Component Development using Various Metal Additive Manufacturing TechniquesThe NASA Marshall Space Flight Center (MSFC) has been involved with various forms of metallic additive manufacturing (AM) for use in liquid rocket engine component design, development, and testing since 2010. These AM techniques have been demonstrated to significantly reduce hardware cost, shorten fabrication schedules, increase reliability by reducing the number of joints, and improve hardware performance by allowing fabrication of designs not feasible by conventional means. The focus at the NASA MSFC for these metal additive manufacturing techniques include laser powder-bed fusion (L-PBF), blown powder directed energy deposition (DED), arc-based deposition, and Laser Wire Direct Closeout (LWDC). A variety of components have been evaluated and tested including thrust chamber injectors, injector components such as faceplates, regeneratively-cooled combustion chambers, regeneratively-cooled nozzles, gas generator and preburner hardware, and augmented spark igniters. To support these component applications in harsh environments, NASA has advanced a variety of “standard” additive manufacturing alloys such as those in the superalloy-family and also evolved new alloys including GRCop-84, GRCop-42, NASA HR-1, and JBK-75. The purpose of this presentation is to discuss the various component programs at the NASA MSFC using AM to develop, fabricate, and test combustion devices hardware and the evolution of the new additive alloys. One of these projects that will be highlighted is Rapid Analysis and Manufacturing Propulsion Technology (RAMPT), which includes new process development for large scale AM components, multi-metallic AM components, including unique component designs using additive manufacturing. Additional information will be provided on the development of other components, hot-fire testing, post-processing of AM techniques including surface enhancements (polishing) techniques, material and process characterization, future development programs, and dissemination of data to industry partners.
Document ID
20205004369
Acquisition Source
Marshall Space Flight Center
Document Type
Presentation
Authors
Paul Gradl
(Marshall Space Flight Center Redstone Arsenal, Alabama, United States)
Chris Protz
(Marshall Space Flight Center Redstone Arsenal, Alabama, United States)
John Fikes
(Marshall Space Flight Center Redstone Arsenal, Alabama, United States)
Dave Ellis
(Glenn Research Center Cleveland, Ohio, United States)
Laura Evans
(Glenn Research Center Cleveland, Ohio, United States)
Date Acquired
July 11, 2020
Subject Category
Spacecraft Propulsion And Power
Meeting Information
Meeting: JANNAF Liquid Propulsion Subcommittee (LPS) Additive Manufacturing for Propulsion Applications Technical Interchange Meeting
Location: Huntsville, AL
Country: US
Start Date: September 28, 2020
End Date: September 30, 2020
Sponsors: United States Department of the Army, United States Department of the Air Force, United States Department of the Navy, National Aeronautics and Space Administration
Funding Number(s)
WBS: 228556.04.22.62
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Technical Review
Single Expert
Keywords
Additive Manufacturing
RAMPT
DED
L-PBF
3D Printing
directed energy deposition
Laser Wire Direct Closeout
GRCop-42
NASA HR-1
Rapid Analysis and Manufacturing Propulsion Technology
Additive
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