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| 报告编号 | NASA-CR-171278, NAS 1.26:171278, QPR-1 |
| 来源ID | NTRS_Document_ID: 19850007463 |
| The investigation of tethered satellite system dynamics | |
| Lorenzini, E. | |
| 英文摘要 | Tethered satellite system (TSS) dynamics were studied. The dynamic response of the TSS during the entire stationkeeping phase for the first electrodynamic mission was investigated. An out of plane swing amplitude and the tether's bowing were observed. The dynamics of the slack tether was studied and computer code, SLACK2, was improved both in capabilities and computational speed. Speed hazard related to tether breakage or plasma contactor failure was examined. Preliminary values of the potential difference after the failure and of the drop of the electric field along the tether axis have been computed. The update of the satellite rotational dynamics model is initiated. |
| 英文关键词 | DYNAMIC RESPONSE ELECTRODYNAMICS SPACE MISSIONS STATIONKEEPING SYSTEMS ENGINEERING TETHERED SATELLITES ARTIFICIAL SATELLITES COMPUTER PROGRAMS DYNAMIC MODELS ELECTRIC FIELDS INPUT/OUTPUT ROUTINES SAFETY MANAGEMENT |
| 出版年 | 1984 |
| 报告类型 | Technical Report |
| 语种 | 英语 |
| 国家 | 美国 |
| URL | http://hdl.handle.net/2060/19850007463 |
| 资源类型 | 科技报告 |
| 条目标识符 | http://119.78.100.177/qdio/handle/2XILL650/259010 |
| 推荐引用方式 GB/T 7714 | Lorenzini, E.. The investigation of tethered satellite system dynamics,1984. |
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