Loading...
Please wait, while we are loading the content...
Similar Documents
Space shuttle maneuvering engine reusable thrust chamber program. task 11: high epsilon injector test report
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Pauckert, R. P. |
| Copyright Year | 1974 |
| Description | A subscale injector test program conducted with a ten-inch diameter like-doublet injector to determine performance and heat flux profiles vs chamber pressure and propellant mixture ratio, and to determine stability characteristics with various acoustic cavity configurations is described. Results are presented. |
| File Size | 686714 |
| Page Count | 37 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19750010243 |
| Archival Resource Key | ark:/13960/t0ht7dc84 |
| Language | English |
| Publisher Date | 1974-12-01 |
| Access Restriction | Open |
| Subject Keyword | Spacecraft Propulsion And Power Injectors Propulsion System Performance Combustion Stability Orbit Maneuvering Engine Space Shuttle Propellant Mass Ratio Fuel Injection Combustion Chambers 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 |
