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Using Innovative Techniques for Manufacturing Rocket Engine HardwareMany of the manufacturing techniques that are currently used for rocket engine component production are traditional methods that have been proven through years of experience and historical precedence. As we enter into a new space age where new launch vehicles are being designed and propulsion systems are being improved upon, it is sometimes necessary to adopt new and innovative techniques for manufacturing hardware. With a heavy emphasis on cost reduction and improvements in manufacturing time, manufacturing techniques such as Direct Metal Laser Sintering (DMLS) are being adopted and evaluated for their use on J-2X, with hopes of employing this technology on a wide variety of future projects. DMLS has the potential to significantly reduce the processing time and cost of engine hardware, while achieving desirable material properties by using a layered powder metal manufacturing process in order to produce complex part geometries. Marshall Space Flight Center (MSFC) has recently hot-fire tested a J-2X gas generator discharge duct that was manufactured using DMLS. The duct was inspected and proof tested prior to the hot-fire test. Using the Workhorse Gas Generator (WHGG) test setup at MSFC?s East Test Area test stand 116, the duct was subject to extreme J-2X gas generator environments and endured a total of 538 seconds of hot-fire time. The duct survived the testing and was inspected after the test. DMLS manufacturing has proven to be a viable option for manufacturing rocket engine hardware, and further development and use of this manufacturing method is recommended.
Document ID
20120002585
Acquisition Source
Marshall Space Flight Center
Document Type
Abstract
Authors
Betts, Erin M.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Reynolds, David C.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Eddleman, David E.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Hardin, Andy
(Engineering Research and Consulting, Inc. Huntsville, AL, United States)
Date Acquired
August 25, 2013
Publication Date
December 5, 2011
Publication Information
Publication: JANNAF 2011 Joint Subcommittee Meeting
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
M11-0615
Report Number: M11-0615
Meeting Information
Meeting: JANNAF Modeling and Simulation Subcommittee
Location: Huntsville, AL
Country: United States
Start Date: December 5, 2011
End Date: December 9, 2011
Sponsors: Department of the Navy, Department of the Navy, Department of the Air Force, Department of the Army
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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