| タイトル | Optimized Heat Interception for Cryogen Tank Support |
| 本文（外部サイト） | http://hdl.handle.net/2060/20080039267 |
| 著者（英） | Canavan, Edgar R.; Miller, F. K. |
| 著者所属（英） | NASA Goddard Space Flight Center |
| 発行日 | 2007-07-16 |
| 言語 | eng |
| 内容記述 | We consider means for using the cooling available in boil-off gas to intercept heat conducted through the support structure of a cryogen tank. A one-dimensional model of the structure coupled to a gas stream gives an analytical expression for heat leak in terms of flow rate for temperature independent-properties and laminar flow. A numerical model has been developed for heat transfer on a thin cylindrical tube with an attached vent line. The model is used to determine the vent path layout that will minimize heat flow into the cryogen tank. The results are useful for a number of applications, but the one of interest in this study is the minimization of the boil-off in large cryopropellant tanks in low Earth and low lunar orbit. |
| NASA分類 | Fluid Mechanics and Thermodynamics |
| 権利 | No Copyright |
