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Combustion dynamics in liquid rocket engines
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | McLain, W. H. |
| Copyright Year | 1971 |
| Description | A chemical analysis of the emission and absorption spectra in the combustion chamber of a nitrogen tetroxide/aerozine-50 rocket engine was conducted. Measurements were made under conditions of preignition, ignition, and post combustion operating periods. The cause of severe ignition overpressures sporadically observed during the vacuum startup of the Apollo reaction control system engine was investigated. The extent to which residual propellants or condensed intermediate reaction products remain after the engine has been operated in a pulse mode duty cycle was determined. |
| File Size | 14719669 |
| Page Count | 284 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19730014163 |
| Archival Resource Key | ark:/13960/t0ms8gm1p |
| Language | English |
| Publisher Date | 1971-09-01 |
| Access Restriction | Open |
| Subject Keyword | Thermodynamics And Combustion Combustion Physics Chemical Analysis Propellant Properties Combustion Products Captive Tests Gas Analysis Liquid Propellant Rocket Engines Combustion Chambers Firing Igniting 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 |
