| タイトル | A Monte Carlo analysis of the Viking lander dynamics at touchdown |
| 本文（外部サイト） | http://hdl.handle.net/2060/19750023452 |
| 著者（英） | Muraca, R. J.; King, C. A.; Campbell, J. W. |
| 著者所属（英） | NASA Langley Research Center |
| 発行日 | 1975-09-01 |
| 言語 | eng |
| 内容記述 | The performance of the Viking lander has been evaluated by using a Monte Carlo simulation, and all results are presented in statistical form. The primary objectives of this analysis were as follows: (1) to determine the three sigma design values of maximum rigid body accelerations and the minimum clearance of the lander body during landing; (2) to determine the probability of an unstable landing; and (3) to determine the probability of the lander body striking a rock. Two configurations were analyzed with the only difference being in the ability of the primary landing gear struts to carry tension loads. |
| NASA分類 | STRUCTURAL MECHANICS |
| レポートNO | 75N31525
L-9830
NASA-TN-D-7959 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/188762 |
