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Additive Manufacturing of Liquid Rocket Engine Combustion Devices: A Summary of Process Developments and Hot-Fire Testing ResultsAdditive Manufacturing (AM) is an emerging technology with a focus on complex metallic component fabrication: Enables complex shapes and internal features that were not possibly with traditional manufacturing techniques, and significant schedule and overall lifecycle cost reductions. To date at the NASA Marshall Space Flight Center (MSFC), combustion devices component hardware ranging in size from 100 - 35,000 lbf has been designed and manufactured using AM and many of these pieces have been hot-fire tested.
Document ID
20180006088
Acquisition Source
Marshall Space Flight Center
Document Type
Presentation
Authors
Gradl, Paul
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Greene, Sandy
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Protz, Chris
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Bullard, Brad
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Buzzell, James
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Garcia, Chance
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Wood, Jessica
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Cooper, Ken
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Hulka, James
(Jacobs Technology, Inc. Huntsville, AL, United States)
Osborne, Robin
(Engineering Research and Consulting (ERC), Inc. Huntsville, AL, United States)
Date Acquired
October 4, 2018
Publication Date
July 9, 2018
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
M18-6850
AIAA Paper 2018-4625
Meeting Information
Meeting: AIAA Joint Propulsion Conference
Location: Cincinnati, OH
Country: United States
Start Date: July 9, 2018
End Date: July 11, 2018
Sponsors: American Inst. of Aeronautics and Astronautics
Distribution Limits
Public
Copyright
Public Use Permitted.
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