| タイトル | Oxygen rich gas generator design and performance analysis |
| 著者（英） | Crawford, R. A.; Gloyer, P. W.; Knuth, W. H. |
| 著者所属（英） | NASA Headquarters |
| 発行日 | 1993-06-01 |
| 言語 | eng |
| 内容記述 | The present oxygen-rich combustion research investigates oxygen gas generator concepts. The theoretical and modeling aspects of a selected concept are presented, together with a refined concept resulting from the findings of the study. This investigation examined a counter-flow gas generator design for O2/H2 mass ratios of 100-200, featuring a near-stoichiometric combustion zone followed by downstream mixing. The critical technologies required to develop a performance model are analyzed and include the following: (1) oxygen flow boiling; (2) two-phase oxygen flow heat transfer; (3) film-cooling in the combustion zone; (4) oxygen-rich combustion with hydrogen; and (5) mixing and dilution. |
| NASA分類 | SPACECRAFT PROPULSION AND POWER |
| レポートNO | 93A49975
AIAA PAPER 93-2159 |
| 権利 | Copyright |
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