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Application of Additively Manufactured Components in Rocket Engine TurbopumpsThe use of additive manufacturing technology has the potential to revolutionize the development of turbopump components in liquid rocket engines. When designing turbomachinery with the additive process there are several benefits and risks that are leveraged relative to a traditional development cycle. This topic explores the details and development of a 90,000 RPM Liquid Hydrogen Turbopump from which 90% of the parts were derived from the additive process. This turbopump was designed, developed and will be tested later this year at Marshall Space Flight Center.
Document ID
20150016257
Acquisition Source
Marshall Space Flight Center
Document Type
Conference Paper
Authors
Calvert, Marty, Jr.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Hanks, Andrew
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Schmauch, Preston
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Delessio, Steve
(Jacobs Engineering and Science Services and Skills Augmentation Group (ESSSA) Huntsville, AL, United States)
Date Acquired
August 21, 2015
Publication Date
June 1, 2015
Subject Category
Mechanical Engineering
Spacecraft Propulsion And Power
Report/Patent Number
M15-4416
Report Number: M15-4416
Meeting Information
Meeting: JANNAF Propulsion Subcommittee Meeting
Location: Nashville, TN
Country: United States
Start Date: June 1, 2015
End Date: June 5, 2015
Sponsors: Johns Hopkins Univ., NASA Headquarters, Department of the Navy, Department of the Army, Department of the Air Force
Distribution Limits
Public
Copyright
Public Use Permitted.
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