NASA NTRS · 19780023221
Liquid rocket engine axial-flow turbopumps
Abstract
The axial pump is considered in terms of the total turbopump assembly. Stage hydrodynamic design, pump rotor assembly, pump materials for liquid hydrogen applications, and safety factors as utilized in state of the art pumps are among the topics discussed. Axial pump applications are included.
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Scheer, D. D., Huppert, M. C., Viteri, F., Farquhar, J., Keller, R. B., Jr.. 1978-04-01. Liquid rocket engine axial-flow turbopumps. https://ntrs.nasa.gov/citations/19780023221
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