NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
SSME main combustion chamber life predictionTypically, low cycle fatigue life is a function of the cyclic strain range, the material properties, and the operating temperature. The reusable life is normally defined by the number of strain cycles that can be accrued before severe material degradation occurs. Reusable life is normally signified by the initiation or propagation of surface cracks. Hot-fire testing of channel wall combustors has shown significant mid-channel wall thinning or deformation during accrued cyclic testing. This phenomenon is termed cyclic-creep and appears to be significantly accelerated at elevated surface temperatures. This failure mode was analytically modelled. The cyclic life of the baseline SSME-MCC based on measured calorimeter heat transfer data, and the life sensitivity of local hot spots caused by injector effects were determined. Four life enhanced designs were assessed.
Document ID
19830027830
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Cook, R. T.
(Rockwell International Corp. Canoga Park, CA, United States)
Fryk, E. E.
(Rockwell International Corp. Canoga Park, CA, United States)
Newell, J. F.
(Rockwell International Corp. Canoga Park, CA, United States)
Date Acquired
September 4, 2013
Publication Date
May 1, 1983
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
RI/RD83-150
NASA-CR-168215
NAS 1.26:168215
Report Number: RI/RD83-150
Report Number: NASA-CR-168215
Report Number: NAS 1.26:168215
Accession Number
83N36101
Funding Number(s)
CONTRACT_GRANT: NAS3-23256
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available