| タイトル | Apollo experience report: Aerothermodynamics evaluation |
| 本文（外部サイト） | http://hdl.handle.net/2060/19720018273 |
| 著者（英） | Lee, D. B. |
| 著者所属（英） | NASA Johnson Space Center |
| 発行日 | 1972-06-01 |
| 言語 | eng |
| 内容記述 | The Apollo program offered the first opportunity to obtain aerothermodynamic measurements at superorbital velocities on full-scale spacecraft. Four unmanned flight tests were conducted to qualify the Apollo command module heat shield. Aerothermodynamic measurements were made, and data are presented to illustrate the comparison of the flight data with the ground-test results and theoretical predictions. |
| NASA分類 | THERMODYNAMICS AND COMBUSTION |
| レポートNO | 72N25923
NASA-TN-D-6843
MSC-S-287 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/203244 |
