| タイトル | Efficient loads analyses of Shuttle-payloads using dynamic models with linear or nonlinear interfaces |
| 著者（英） | Spanos, P. D.; Cao, T. T.; Hamilton, D. A.; Nelson, D. A. R. |
| 著者所属（英） | Rice Univ.|Lockheed Engineering and Sciences Co.|NASA Johnson Space Center |
| 発行日 | 1989-01-01 |
| 言語 | eng |
| 内容記述 | An efficient method for the load analysis of Shuttle-payload systems with linear or nonlinear attachment interfaces is presented which allows the kinematics of the interface degrees of freedom at a given time to be evaluated without calculating the combined system modal representation of the Space Shuttle and its payload. For the case of a nonlinear dynamic model, an iterative procedure is employed to converge the nonlinear terms of the equations of motion to reliable values. Results are presented for a Shuttle abort landing event. |
| NASA分類 | LAUNCH VEHICLES AND SPACE VEHICLES |
| レポートNO | 89A30693
AIAA PAPER 89-1203 |
| 権利 | Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/364678 |
