| タイトル | Apollo Lunar Module Landing Gear |
| 本文（外部サイト） | http://hdl.handle.net/2060/19730010151 |
| 著者（英） | Rogers, W. F. |
| 著者所属（英） | NASA Johnson Space Center |
| 発行日 | 1972-11-01 |
| 言語 | eng |
| 内容記述 | The Apollo lunar module landing-gear flight-performance results and three principal gear development problems are discussed. In evaluating the lunar module touchdown performance, strut stroking and toppling stability are the prime factors and are governed primarily by touchdown velocity and surface slope at the touchdown point. Flight results are shown to be well within design values, and the landing-gear has performed successfully in all landings. |
| NASA分類 | SPACE VEHICLES |
| レポートNO | 73N18878 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/570574 |
