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Space shuttle maneuvering engine reusable thrust chamber program. task 11: low epsilon stability test report data dump
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Pauckert, R. P. |
| Copyright Year | 1974 |
| Description | The stability characteristics of the like-doublet injector were defined over the range of OME chamber pressures and mixture ratios. This was accomplished by bomb testing the injector and cavity configurations in solid wall thrust chamber hardware typical of a flight contour with fuel heated to regenerative chamber outlet temperatures. It was found that stability in the 2600-2800 Hz region depends upon injector hydraulics and on chamber acoustics. |
| File Size | 914450 |
| Page Count | 29 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19750003997 |
| Archival Resource Key | ark:/13960/t9h46h798 |
| Language | English |
| Publisher Date | 1974-01-01 |
| Access Restriction | Open |
| Subject Keyword | Spacecraft Propulsion And Power Stability Tests Space Shuttles Thrust Chambers Cavitation Flow Hardware Inlet Flow Fuel Injection Fuel-air Ratio Regenerative Cooling 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 |
