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Space shuttle maneuvering engine reusable thrust chamber program. task 11: stability analyses and acoustic model testing data dump
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Oberg, C. L. |
| Copyright Year | 1974 |
| Description | The combustion stability characteristics of engines applicable to the Space Shuttle Orbit Maneuvering System and the adequacy of acoustic cavities as a means of assuring stability in these engines were investigated. The study comprised full-scale stability rating tests, bench-scale acoustic model tests and analysis. Two series of stability rating tests were made. Acoustic model tests were made to determine the resonance characteristics and effects of acoustic cavities. Analytical studies were done to aid design of the cavity configurations to be tested and, also, to aid evaluation of the effectiveness of acoustic cavities from available test results. |
| File Size | 1635761 |
| Page Count | 47 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19750010242 |
| Archival Resource Key | ark:/13960/t1tf4k97z |
| Language | English |
| Publisher Date | 1974-12-01 |
| Access Restriction | Open |
| Subject Keyword | Spacecraft Propulsion And Power Performance Tests Resonant Frequencies Combustion Stability Orbit Maneuvering Engine Space Shuttle Systems Analysis Rocket Engine Design Propellant Combustion System Effectiveness 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 |
