NASA NTRS · 20010020158
Unshrouded Impeller Technology Development Status
Abstract
To 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.
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Droege, Alan R., Williams, Robert W., Garcia, Roberto. 2000-01-01. Unshrouded Impeller Technology Development Status. https://ntrs.nasa.gov/citations/20010020158
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