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Nozzle extension design status reportTwenty possible concepts of a possible nozzle/nozzle extension interface were originated. Not all of the concepts were considered worthy of analysis time. Six of them were thermally analyzed and three were stress analyzed. These analyses were done to determine which of the concepts would have the best chance of succeeding, that is, they were a screening process which was to allow rating of one concept against another. This was done because adequate material properties to determine absolute stress levels were not available at the time of the analyses. Through all of the concepts still exhibit some areas of negative margin of safety, concept no. 1 shows good promise that, with slight modifications, it could have all positive margins of safety. Another significant question, regarding these designs, has to do with the Grafoil seals and insulators. Some additional data was just recently received on Grafoil properties, but it was too late to incorporate in the analyses. The new data were not significantly different from the properties which were used.
Document ID
19730015597
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Classen, L. B.
(Aerojet Nuclear Systems Co. Azusa, CA, United States)
Date Acquired
September 2, 2013
Publication Date
May 1, 1972
Subject Category
Fluid Mechanics
Report/Patent Number
NASA-CR-132211
N8500:72-143-F-398-7
Report Number: NASA-CR-132211
Report Number: N8500:72-143-F-398-7
Accession Number
73N24324
Funding Number(s)
PROJECT: PROJ. 143
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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