| タイトル | Apollo experience report: Structural loads due to maneuvers of the command and service module/lunar module |
| 本文（外部サイト） | http://hdl.handle.net/2060/19720012256 |
| 著者（英） | Rutkowski, M. J. |
| 著者所属（英） | NASA Johnson Space Center |
| 発行日 | 1972-03-01 |
| 言語 | eng |
| 内容記述 | Analyses were performed to determine the structural loads caused by maneuvers of the docked Apollo command and service module/lunar module (CSM/LM). Results of CSM/LM docked interface loads analyses and service-propulsion-system engine support structure load analyses are compared with the structural allowable loads of the CSM/LM docked interface and the service-propulsion-system engine thrust mount, respectively, for different phases of spaceflight operations. An analysis also was performed to investigate the loads that resulted from the failure case in which the LM descent propulsion system is started in the full-throttle position. |
| NASA分類 | SPACE VEHICLES |
| レポートNO | 72N19906
NASA-TN-D-6719
MSC-S-280 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/203873 |
