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Structural dynamic analysis of the space shuttle main engine
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Scott, L. P. McCutcheon, W. A. Jamison, G. T. Price, J. M. |
| Copyright Year | 1981 |
| Description | This structural dynamic analysis supports development of the SSME by evaluating components subjected to critical dynamic loads, identifying significant parameters, and evaluating solution methods. Engine operating parameters at both rated and full power levels are considered. Detailed structural dynamic analyses of operationally critical and life limited components support the assessment of engine design modifications and environmental changes. Engine system test results are utilized to verify analytic model simulations. The SSME main chamber injector assembly is an assembly of 600 injector elements which are called LOX posts. The overall LOX post analysis procedure is shown. |
| File Size | 47802845 |
| Page Count | 166 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19820011428 |
| Archival Resource Key | ark:/13960/t2t48hp1v |
| Language | English |
| Publisher Date | 1981-12-01 |
| Access Restriction | Open |
| Subject Keyword | Space Transportation Dynamic Structural Analysis Fatigue Life Stress Analysis Injectors Liquid Oxygen Space Shuttle Main Engine Thermal Cycling Tests Mathematical Models Dynamic Loads Engine Tests Parameter Identification Static Loads Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
