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Coaxial propellant injectors with faceplate annulus control
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Miyata, Shinjiro Horn, Mark D. Farhangi, Shahram |
| Copyright Year | 2010 |
| Description | An improved design concept for coaxial propellant injectors for a rocket engine (or perhaps for a non-rocket combustion chamber) offers advantages of greater robustness, less complexity, fewer parts, lower cost, and less bulk, relative to prior injectors of equivalent functionality. This design concept is particularly well suited to small, tight-tolerance injectors, for which prior designs are not suitable because the practical implementation of those designs entails very high costs and difficulty in adhering to the tolerances. |
| File Size | 133394 |
| Page Count | 1 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_20100012813 |
| Archival Resource Key | ark:/13960/t75t8mm8z |
| Language | English |
| Publisher Date | 2010-04-01 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Propulsion And Power Propellants Injectors Coaxial Flow Rocket Engines Fuel Injection Combustion Chambers Annular Flow 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 |
