| タイトル | System analysis approach to deriving design criteria (loads) for Space Shuttle and its payloads. Volume 1: General statement of approach |
| 本文（外部サイト） | http://hdl.handle.net/2060/19820006330 |
| 著者（英） | Bullock, T.; Holland, W. B.; Kiefling, L. A.; Kross, D. A.; Ryan, R. S. |
| 著者所属（英） | NASA Marshall Space Flight Center |
| 発行日 | 1981-12-01 |
| 言語 | eng |
| 内容記述 | Space shuttle, the most complex transportation system designed to date, illustrates the requirement for an analysis approach that considers all major disciplines simultaneously. Its unique cross coupling and high sensitivity to aerodynamic uncertainties and high performance requirements dictated a less conservative approach than those taken in programs. Analyses performed for the space shuttle and certain payloads, Space Telescope and Spacelab, are used a examples. These illustrate the requirements for system analysis approaches and criteria, including dynamic modeling requirements, test requirements control requirements and the resulting design verification approaches. A survey of the problem, potential approaches available as solutions, implications for future systems, and projected technology development areas are addressed. |
| NASA分類 | LAUNCH VEHICLES AND SPACE VEHICLES |
| レポートNO | 82N14203
M-358
NASA-TP-1949 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/167380 |
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