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Composite load spectra for select space propulsion structural componentsThe objective of this program is to develop generic load models with multiple levels of progressive sophistication to simulate the composite load spectra that are induced in space propulsion system components, representative of Space Shuttle Main Engines (SSME), such as transfer ducts, turbine blades, and liquid oxygen (LOX) posts and system ducting. These models will be developed using two independent approaches. The first approach consists of using state-of-the-art probabilistic methods to describe the individual loading conditions and combinations of these loading conditions to synthesize the composite load spectra simulation. The methodology required to combine the various individual load simulation models (hot-gas dynamic, vibrations, instantaneous position, centrifugal field, etc.) into composite load spectra simulation models will be developed under this program. A computer code incorporating the various individual and composite load spectra models will be developed to construct the specific load model desired. The second approach, which is covered under the options portion of the contract, will consist of developing coupled models for composite load spectra simulation which combine the (deterministic) models for composite load dynamic, acoustic, high-pressure and high rotational speed, etc., load simulation using statistically varying coefficients. These coefficients will then be determined using advanced probabilistic simulation methods with and without strategically selected experimental data. This report covers the efforts of the third year of the contract. The overall program status is that the turbine blade loads have been completed and implemented. The transfer duct loads are defined and are being implemented. The thermal loads for all components are defined and coding is being developed. A dynamic pressure load model is under development. The parallel work on the probabilistic methodology is essentially completed. The overall effort is being integrated in an expert system code specifically developed for this project.
Document ID
19920007126
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Newell, J. F.
(Rockwell International Corp. Canoga Park, CA, United States)
Kurth, R. E.
(Rockwell International Corp. Canoga Park, CA, United States)
Ho, H.
(Rockwell International Corp. Canoga Park, CA, United States)
Date Acquired
September 6, 2013
Publication Date
November 1, 1991
Subject Category
Structural Mechanics
Report/Patent Number
NASA-CR-189049
NAS 1.26:189049
Report Number: NASA-CR-189049
Report Number: NAS 1.26:189049
Accession Number
92N16344
Funding Number(s)
PROJECT: RTOP 505-13-00
CONTRACT_GRANT: NAS3-24382
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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