| タイトル | The staging dynamics of a proposed space shuttle configuration |
| 本文（外部サイト） | http://hdl.handle.net/2060/19730009159 |
| 著者（英） | Hamilton, D. A. |
| 著者所属（英） | NASA Johnson Space Center |
| 発行日 | 1972-10-01 |
| 言語 | eng |
| 内容記述 | A mathematical model was developed to simulate the staging dynamics of a proposed space shuttle configuration. Included in the mathematical model is the kinematics and dynamics of the staging mechanism, thrust forces and thrust vector control, rigid-body dynamics, and structural dynamics of both the booster and orbiter stages of the configuration. The mathematical model was incorporated into a computer program so that the staging maneuver could be simulated. Results of the simulations are presented. |
| NASA分類 | SPACE VEHICLES |
| レポートNO | 73N17886
NASA-TM-X-58098
MSC-07236 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/200517 |
