| タイトル | RQL Integrated Module Rig Test |
| 本文（外部サイト） | http://hdl.handle.net/2060/20040033929 |
| 著者（英） | Padget, Frederick C., IV; Holdeman, James D.; Koopman, Frederick S.; Ols, John T.; Siskind, Kenneth S. |
| 著者所属（英） | Pratt and Whitney Aircraft Group |
| 発行日 | 2004-02-01 |
| 言語 | eng |
| 内容記述 | This report documents the activities conducted under Work Breakdown Structure (WBS) 1.0.2.7 of the NASA Critical Components (CPC) Program to evaluate the low emissions potential of a Rich-Quench-Lean combustor capable of achieving the program goal of emissions of nitrogen oxides (NOxEI) less than 5 gm/Kg fuel at the supersonic light condition while maintaining combustion efficiencies in excess of 99.9 percent. The chosen combustor module would then be tested in the subscale annular rig test prior to testing in the subscale core engine demonstrator, if the RQL concept were to be chosen at the Combustor Downselect. |
| NASA分類 | Aircraft Propulsion and Power |
| レポートNO | NASA/CR-2004-212881
MTD211A5
E-14295 |
| 権利 | No Copyright |
