| タイトル | Reusable Launch Vehicle Tank/Intertank Sizing Trade Study |
| 本文（外部サイト） | http://hdl.handle.net/2060/20000032922 |
| 著者（英） | Myers, David E.; Dorsey, John T.; Martin, Carl J. |
| 著者所属（英） | NASA Langley Research Center |
| 発行日 | 2000-01-01 |
| 言語 | eng |
| 内容記述 | A tank and intertank sizing tool that includes effects of major design drivers, and which allows parametric studies to be performed, has been developed and calibrated against independent representative results. Although additional design features, such as bulkheads and field joints, are not currently included in the process, the improved level of fidelity has allowed parametric studies to be performed which have resulted in understanding of key tank and intertank design drivers, design sensitivities, and definition of preferred design spaces. The sizing results demonstrated that there were many interactions between the configuration parameters of internal/external payload, vehicle fineness ratio (half body angle), fuel arrangement (LOX-forward/LOX-aft), number of tanks, and tank shape/arrangement (number of lobes). |
| NASA分類 | Launch Vehicles and Launch Operations |
| レポートNO | AIAA Paper 2000-1043 |
| 権利 | Copyright, Distribution as joint owner in the copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/95031 |
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