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Investigation of characteristics of feed system instabilitiesThe relationship between the structural and feed system natural frequencies in structure-propulsion system coupled longitudinal oscillations (pogo) is investigated. The feed system frequencies are usually very dependent upon the compressibility (compliance) of cavitation bubbles that exist to some extent in all operating turbopumps. This document includes: a complete review of cavitation mechanisms; development of a turbopump cavitation compliance model; an accumulation and analysis of all available cavitation compliance test data; and a correlation of empirical-analytical results. The analytical model is based on the analysis of flow relative to a set of cascaded blades, having any described shape, and assumes phase changes occur under conditions of isentropic equilibrium. Analytical cavitation compliance predictions for the J-2 LOX, F-1 LOX, H-1 LOX and LR87 oxidizer turbopump inducers do not compare favorably with test data. The model predicts much less cavitation than is derived from the test data. This implies that mechanisms other than blade cavitation contribute significantly to the total amount of turbopump cavitation.
Document ID
19720022122
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Vaage, R. D.
(Martin Marietta Corp. Denver, CO, United States)
Fidler, L. E.
(Martin Marietta Corp. Denver, CO, United States)
Zehnle, R. A.
(Martin Marietta Corp. Denver, CO, United States)
Date Acquired
August 6, 2013
Publication Date
May 1, 1972
Subject Category
Propellants
Report/Patent Number
MCR-72-107
NASA-CR-123752
Report Number: MCR-72-107
Report Number: NASA-CR-123752
Accession Number
72N29772
Funding Number(s)
CONTRACT_GRANT: NAS8-26266
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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