| タイトル | Analysis and test for space shuttle propellant dynamics |
| 本文（外部サイト） | http://hdl.handle.net/2060/19830022244 |
| 著者（英） | Demchak, L. J.; Berry, R. L.; Tegart, J. R. |
| 著者所属（英） | Martin Marietta Aerospace |
| 発行日 | 1983-06-01 |
| 言語 | eng |
| 内容記述 | This report presents the results of a study to develop an analytical model capable of predicting the dynamic interaction forces on the Shuttle External Tank, due to large amplitude propellant slosh during RTLS separation. The report details low-g drop tower and KC-135 test programs that were conducted to investigate propellant reorientation during RTLS. In addition, the development of a nonlinear finite element slosh model (LAMPS2, two dimensional, and one LAMPS3, three dimensional) is presented. Correlation between the model and test data is presented as a verification of the modeling approach. |
| NASA分類 | SPACECRAFT PROPULSION AND POWER |
| レポートNO | 83N30515
NAS 1.26:3683
NASA-CR-3683
MCR-81-528 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/161963 |
