NASA NTRS · 19750012398
Turbopump systems for liquid rocket engines
Abstract
The turbopump system, from preliminary design through rocket engine testing is examined. Selection of proper system type for each application and integration of the components into a working system are dealt with. Details are also given on the design of various components including inducers, pumps, turbines, gears, and bearings.
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1974-08-01. Turbopump systems for liquid rocket engines. https://ntrs.nasa.gov/citations/19750012398
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