NASA NTRS · 19730015803
LH2 pump component development testing in the electric pump room at test cell C inducer no. 1
Abstract
The characteristics of a turbine pump for use with the nuclear engine for rocket vehicles are discussed. It was determined that the pump will be a two stage centrifugal pump with both stages having backswept impellers and an inducer upstream of the first stage impeller. The test program provided demonstration of the ability of the selected design to meet the imposed requirements.
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Andrews, F. X., Brunner, J. J., Kirk, K. G., Mathews, J. P., Nishioka, T.. 1972-05-01. LH2 pump component development testing in the electric pump room at test cell C inducer no. 1. https://ntrs.nasa.gov/citations/19730015803
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