| タイトル | Effect of Propellant Flowrate and Purity on Carbon Deposition in LO2/Methane Gas Generators |
| 本文（外部サイト） | http://hdl.handle.net/2060/19900009152 |
| 著者（英） | Bossard, J. A.; Braam, F.; Niiya, K. Y.; Burkhardt, W. M. |
| 著者所属（英） | NASA Marshall Space Flight Center |
| 発行日 | 1989-05-01 |
| 言語 | eng |
| 内容記述 | The generation and deposition of carbon was studied in the Carbon Deposition Program using subscale hardware with LO2/Liquid Natural Gas (LNG) and LO2/Methane propellants at low mixture ratios. The purpose of the testing was to evaluate the effect of methane purity and full scale injection density on carbon deposition. The LO2/LNG gas generator/preburner testing was performed at mixture ratios between 0.24 and 0.58 and chamber pressures from 5.8 to 9.4 MPa (840 to 1370 psia). A total of seven 200 second duration tests were performed. The LNG testing occurred at low injection densities, similar to the previous LO2/RP-1, LO2/propane, and LO2/methane testing performed on the carbon deposition program. The current LO2/methane test series occurred at an injection density factor of approximately 10 times higher than the previous testing. The high injection density LO2/methane testing was performed at mixture ratios between from 0.23 to 0.81 and chamber pressures from 6.4 to 15.2 MPa (925 to 2210 psia). A total of nine high injection density tests were performed. The testing performed demonstrated that low purity methane (LNG) did not produce any detectable change in carbon deposition when compared to pure methane. In addition, the C* performance and the combustion gas temperatures measured were similar to those obtained for pure methane. Similar results were obtained testing pure methane at higher propellant injection densities with coarse injector elements. |
| NASA分類 | SPACECRAFT PROPULSION AND POWER |
| レポートNO | 90N18468 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/138901 |
