Publication Date:
2019-06-27
Description:
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.
Keywords:
MACHINE ELEMENTS AND PROCESSES
Type:
NASA-CR-132232
,
N8300R:72-101
Format:
application/pdf
Permalink