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Three dimensional thrust chamber life predictionA study was performed to analytically determine the cyclic thermomechanical behavior and fatigue life of three configurations of a Plug Nozzle Thrust Chamber. This thrust chamber is a test model which represents the current trend in nozzle design calling for high performance coupled with weight and volume limitations as well as extended life for reusability. The study involved the use of different materials and material combinations to evaluate their application to the problem of low-cycle fatigue in the thrust chamber. The thermal and structural analyses were carried out on a three-dimensional basis. Results are presented which show plots of continuous temperature histories and temperature distributions at selected times during the operating cycle of the thrust chamber. Computed structural data show critical regions for low-cycle fatigue and the histories of strain within the regions for each operation cycle.
Document ID
19760012141
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Armstrong, W. H.
(Boeing Aerospace Co. Seattle, WA, United States)
Brogren, E. W.
(Boeing Aerospace Co. Seattle, WA, United States)
Date Acquired
September 3, 2013
Publication Date
March 1, 1976
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
D180-19309-1
NASA-CR-134979
Report Number: D180-19309-1
Report Number: NASA-CR-134979
Accession Number
76N19229
Funding Number(s)
CONTRACT_GRANT: NAS3-19717
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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