| タイトル | Radiator design system computer programs |
| 本文（外部サイト） | http://hdl.handle.net/2060/19730015219 |
| 著者（英） | Wiggins, C. L.; Oren, J. A.; Dietz, J. B. |
| 著者所属（英） | Vought Missiles and Space Co. |
| 発行日 | 1971-10-13 |
| 言語 | eng |
| 内容記述 | Minimum weight space radiator subsystems which can operate over heat load ranges wider than the capabilities of current subsystems are investigated according to projected trends of future long duration space vehicles. Special consideration is given to maximum heat rejection requirements of the low temperature radiators needed for environmental control systems. The set of radiator design programs that have resulted from this investigation are presented in order to provide the analyst with a capability to generate optimum weight radiator panels or sets of panels from practical design considerations, including transient performance. Modifications are also provided for existing programs to improve capability and user convenience. |
| NASA分類 | THERMODYNAMICS AND COMBUSTION |
| レポートNO | 73N23946
NASA-CR-128913 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/199180 |
