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SRM Internal Flow Tests and Computational Fluid Dynamic AnalysisThis document presents the full-scale analyses of the CFD RSRM. The RSRM model was developed with a 20 second burn time. The following are presented as part of the full-scale analyses: (1) RSRM embedded inclusion analysis; (2) RSRM igniter nozzle design analysis; (3) Nozzle Joint 4 erosion anomaly; (4) RSRM full motor port slag accumulation analysis; (5) RSRM motor analysis of two-phase flow in the aft segment/submerged nozzle region; (6) Completion of 3-D Analysis of the hot air nozzle manifold; (7) Bates Motor distributed combustion test case; and (8) Three Dimensional Polysulfide Bump Analysis.
Document ID
20010110105
Acquisition Source
Marshall Space Flight Center
Document Type
Other
Date Acquired
September 7, 2013
Publication Date
October 30, 2001
Subject Category
Fluid Mechanics And Thermodynamics
Report/Patent Number
ERC/HSV-TR01-01-Vol-2
Funding Number(s)
CONTRACT_GRANT: NAS8-40347
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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