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NERVA nozzle design status reportThe results of the design analyses are presented along with the status of the attained design maturity of the structural elements of the nozzle jacket and various aspects of the coolant passages. The design analyses relating to the nozzle shell were based on design allowables as supported by cursory values obtained from ARMCO 22-13-5 nozzle forgings. The major aspects of the coolant passages considered include: low cycle thermal fatigue, ability to operate at 4500 R gas temperature, tube buckling, and susceptibility to erosion. The scope of the analysis is limited to processes leading to reliability assessments of failure mechanisms.
Document ID
19730015942
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Williams, J. J.
(Aerojet Nuclear Systems Co. Azusa, CA, United States)
Pickering, J. L.
(Aerojet Nuclear Systems Co. Azusa, CA, United States)
Ackerman, R. G.
(Aerojet Nuclear Systems Co. Azusa, CA, United States)
Date Acquired
September 2, 2013
Publication Date
May 1, 1972
Subject Category
Nuclear Engineering
Report/Patent Number
NASA-CR-132223
N8500:72-141-F-198-1
Report Number: NASA-CR-132223
Report Number: N8500:72-141-F-198-1
Accession Number
73N24669
Funding Number(s)
PROJECT: PROJ. 141
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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