| タイトル | Injector design guidelines for gas/liquid propellant systems |
| 本文（外部サイト） | http://hdl.handle.net/2060/19730013999 |
| 著者（英） | Falk, A. Y.; Burick, R. J. |
| 著者所属（英） | Rockwell International Corp. |
| 発行日 | 1973-05-01 |
| 言語 | eng |
| 内容記述 | Injector design guidelines are provided for gas/liquid propellant systems. Information was obtained from a 30-month applied research program encompassing an analytical, design, and experimental effort to relate injector design parameters to simultaneous attainment of high performance and component (injector/thrust chamber) compatibility for gas/liquid space storable propellants. The gas/liquid propellant combination studied was FLOX (82.6% F2)/ ambient temperature gaseous methane. Design criteria that provide for simultaneous attainment of high performance and chamber compatibility are presented for both injector types. Parametric data are presented that are applicable for the design of circular coaxial and like-doublet injectors that operate with design parameters similar to those employed. However, caution should be exercised when applying these data to propellant combinations whose elements operate in ranges considerably different from those employed in this study. |
| NASA分類 | PROPULSION SYSTEMS |
| レポートNO | 73N22726
R-8973-3
NASA-CR-120968 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/199390 |
