| タイトル | Radiative heating to the Apollo command module: Engineering prediction and flight measurement |
| 本文（外部サイト） | http://hdl.handle.net/2060/19720017314 |
| 著者（英） | Milhoan, J. D.; Rochelle, W. C.; Ried, R. C., Jr. |
| 著者所属（英） | NASA Johnson Space Center |
| 発行日 | 1972-04-01 |
| 言語 | eng |
| 内容記述 | The theory and engineering techniques used for the prediction of the Apollo entry thermal-radiation environment are presented. The radiation predictions are shown to be in satisfactory agreement with the Apollo 4, FIRE 1, and FIRE 2 flight radiometer data. The characteristics and performance of the Apollo flight radiometer and ablator-mounted configuration were determined through arc jet simulation tests. |
| NASA分類 | THERMODYNAMICS AND COMBUSTION |
| レポートNO | 72N24964
NASA-TM-X-58091
MSC-06834 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/203357 |
