| タイトル | Design of propellant acquisition systems for advanced cryogenic space propulsion systems |
| 著者（英） | Burge, G. W.; Castle, J. N.; Blackmon, J. B. |
| 発行日 | 1973-11-01 |
| 言語 | eng |
| 内容記述 | This paper presents results of work conducted to expand the technology base and evolve practical propellant surface tension acquisition system designs for future cryogenic space vehicles. Surface tension screen device channel flow analysis and supporting tests showed that reasonable mesh sizes could provide the required retention performance. Integrated subsystem studies and development showed that practical and effective screen surface tension acquisition devices could be designed for typical applications, but that other interfacing feed subsystems are often constrained by the design of the particular acquisition device. These constraints may dominate the total feed system performance. |
| NASA分類 | SPACE VEHICLES |
| レポートNO | 74A11296
AIAA PAPER 73-1287 |
| 権利 | Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/454949 |
