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Advanced Manufacturing Technologies (AMT): Additive Manufactured Hot Fire Planning and Testing in GRC Cell 32 ProjectThe objective of this project is to hot fire test an additively manufactured thrust chamber assembly TCA (injector and thrust chamber). GRC will install the additively manufactured Inconel 625 injector, two additively manufactured (SLM) water cooled Cu-Cr thrust chamber barrels and one additively manufactured (SLM) water cooled Cu-Cr thrust chamber nozzle on the test stand in Cell 32 and perform hot fire testing of the integrated TCA.
Document ID
20140016692
Acquisition Source
Marshall Space Flight Center
Document Type
Other
Authors
Fikes, John C. (NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
November 24, 2014
Publication Date
September 5, 2014
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
M14-4125
Report Number: M14-4125
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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