| タイトル | Design and assembly sequence analysis of option 3 for CETF reference space station |
| 本文（外部サイト） | http://hdl.handle.net/2060/19880003987 |
| 著者（英） | Garrett, L. Bernard; Hall, John B., Jr.; Allen, Cheryl L.; So, Kenneth T.; Andersen, Gregory C.; Scott, A. D., Jr. |
| 著者所属（英） | NASA Langley Research Center |
| 発行日 | 1987-11-01 |
| 言語 | eng |
| 内容記述 | A design and assembly sequence was conducted on one option of the Dual Keel Space Station examined by a NASA Critical Evaluation Task Force to establish viability of several variations of that option. A goal of the study was to produce and analyze technical data to support Task Force decisions to either examine particular Option 3 variations in more depth or eliminate them from further consideration. An analysis of the phasing assembly showed that use of an Expendable Launch Vehicle in conjunction with the Space Transportation System (STS) can accelerate the buildup of the Station and ease the STS launch rate constraints. The study also showed that use of an Orbital Maneuvering Vehicle on the first flight can significantly benefit Station assembly and, by performing Station subsystem functions, can alleviate the need for operational control and reboost systems during the early flights. In addition to launch and assembly sequencing, the study assessed stability and control, and analyzed node-packaging options and the effects of keel removal on the structural dynamics of the Station. Results of these analyses are presented and discussed. |
| NASA分類 | LAUNCH VEHICLES AND SPACE VEHICLES |
| レポートNO | 88N13369
NAS 1.15:100503
NASA-TM-100503 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/148096 |
