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High performance n204/amine elements: blowapart. [test, and analysis of single element injectors
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Lawver, B. R. |
| Copyright Year | 1974 |
| Description | The work is reported which was conducted to define the mechanisms governing blowapart of hypergolic propellant through the design, fabrication, test, and analysis of single element injectors. Data were developed that show the parameters exhibiting a controlling influence over blowapart are the chamber pressure, orifice diameter, and propellant temperature. Mixing, popping (cyclic blowapart), low pressure separation, and high pressure separation were identified as modes of reactive impingement. |
| File Size | 7574135 |
| Page Count | 44 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19750022253 |
| Archival Resource Key | ark:/13960/t8x97033x |
| Language | English |
| Publisher Date | 1974-11-15 |
| Access Restriction | Open |
| Subject Keyword | Propellants And Fuels Nozzle Design Injectors Scale Models Impingement Space Tugs Hypergolic Rocket Propellants Parameterization Separated 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 |
