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Flow induced vibrations in the ssme injector heads
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Lepore, Frank A. |
| Copyright Year | 1991 |
| Description | A description is given of the flowfield in the Space Shuttle Main Engine (SSME) powerhead, the mechanisms which control flow-induced vibrations, and previous experimental work. An in-depth description is given of the development phase of the program , which includes the analysis, design, and fabrication of liquid oxygen (LOX) posts models used in the experimental phase, as well as test facilities, equipment, and procedures used. Also covered is the experimental data analysis, which includes overall steady state powerhead flowfield as well as the high frequency response of the LOX posts. |
| File Size | 3833416 |
| Page Count | 92 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19910021900 |
| Archival Resource Key | ark:/13960/t6qz74w0k |
| Language | English |
| Publisher Date | 1991-06-01 |
| Access Restriction | Open |
| Subject Keyword | Spacecraft Propulsion And Power Fabrication Test Facilities Vibration Injectors Liquid Oxygen Space Shuttle Main Engine Flow Distribution High Frequencies Steady State 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 |
