| タイトル | Orbiter Landing Loads Math Model Description and Correlation with ALT Flight Data |
| 本文（外部サイト） | http://hdl.handle.net/2060/19800007831 |
| 著者（英） | Hamilton, D. A.; Schliesing, J. A.; Zupp, G. A., Jr. |
| 著者所属（英） | NASA Johnson Space Center |
| 発行日 | 1980-01-01 |
| 言語 | eng |
| 内容記述 | Results of the space shuttle approach and landing test are examined in order to assess landing gear characteristics and performance and verify landing dynamic analyses. The landing gears were instrumented with load-calibrated strain gages, a wheel-speed sensor, and strut stroke measurement devices. The mathematical procedure used in predicting the shuttle touchdown loads and dynamics is presented together with the comparisons between measured flight data and the analytical predictions. Conclusions from these data are also presented. |
| NASA分類 | SPACECRAFT DESIGN, TESTING AND PERFORMANCE |
| レポートNO | 80N16091
NASA-RP-1056
JSC-16202
S-498 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/173550 |
