| タイトル | Transient response of a high-capacity heat pipe for Space Station Freedom |
| 著者（英） | Holmes, H. R.; Ambrose, J. H. |
| 著者所属（英） | Lockheed Missiles and Space Co. |
| 発行日 | 1991-06-01 |
| 言語 | eng |
| 内容記述 | High-capacity heat pipe radiator panels have been proposed as the primary means of heat rejection for Space Station Freedom. In this system, the heat pipe would interface with the thermal bus condensers. Changes in system heat load can produce large temperature and heat load variations in individual heat pipes. Heat pipes could be required to start from an initially cold state, with heat loads temporarily exceeding their low-temperature transport capacity. The present research was motivated by the need for accurate prediction of such transient operating conditions. In this work, the cold startup of a 6.7-meter long high-capacity heat pipe is investigated experimentally and analytically. A transient thermohydraulic model of the heat pipe was developed which allows simulation of partially-primed operation. The results of cold startup tests using both constant temperature and constant heat flux evaporator boundary conditions are shown to be in good agreement with predicted transient response. |
| NASA分類 | FLUID MECHANICS AND HEAT TRANSFER |
| レポートNO | 91A43465
AIAA PAPER 91-1403 |
| 権利 | Copyright |
