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Unshrouded Impeller Technology Development StatusTo increase payload and decrease the cost of future Reusable Launch Vehicles (RLVs), engineers at NASA/MSFC and Boeing, Rocketdyne are developing unshrouded impeller technology for application to rocket turbopumps. An unshrouded two-stage high-pressure fuel pump is being developed to meet the performance objectives of a three-stage shrouded pump. The new pump will have reduced manufacturing costs and pump weight. The lower pump weight will allow for increased payload.
Document ID
20010020158
Acquisition Source
Marshall Space Flight Center
Document Type
Conference Paper
Authors
Droege, Alan R.
(NASA Marshall Space Flight Center Huntsville, AL United States)
Williams, Robert W.
(NASA Marshall Space Flight Center Huntsville, AL United States)
Garcia, Roberto
(NASA Marshall Space Flight Center Huntsville, AL United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 2000
Subject Category
Mechanical Engineering
Meeting Information
Meeting: PERC Prolusion Symposium
Location: Cleveland,OH
Country: United States
Start Date: October 26, 2000
End Date: October 27, 2000
Sponsors: Political Economy Research Center
Funding Number(s)
CONTRACT_GRANT: NRA8-21
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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