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High performance n2o4/amine elements blowapart
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Lawver, B. R. |
| Copyright Year | 1979 |
| Description | An experimental and analytical program was conducted to develop an understanding of the mechanisms controlling hypergolic propellant reactive stream separation (RSS). RSS is a combustion induced phenomenon that results in striation of hypergolic propellant oxidizer and fuel sprays fans. This reduced intraelement mixing can influence thrust chamber performance, heat transfer, and stability. The program and product were the development of design criteria for coping with RSS to allow the design of high performance, stable injectors. |
| File Size | 1658072 |
| Page Count | 49 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19790019152 |
| Archival Resource Key | ark:/13960/t04z03f93 |
| Language | English |
| Publisher Date | 1979-03-01 |
| Access Restriction | Open |
| Subject Keyword | Propellants And Fuels Fractionation Mixing Pressure Effects Amines Injectors Space Shuttles Liquid Rocket Propellants Nitrogen Tetroxide Parameterization Boundary Layer Separation Temperature Effects Flow Distribution Flow Velocity Separated Flow Combustion Efficiency Graphs Charts 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 |
