| タイトル | Space Station multidisciplinary analysis capability - IDEAS2 |
| 著者（英） | Habermeyer, J. A.; Johnson, C. L.; Hipol, P. J.; Deryder, L. J.; Chiger, H. D.; Baker, M. |
| 著者所属（英） | NASA Langley Research Center|Structural Dynamics Research Corp. |
| 発行日 | 1986-01-01 |
| 言語 | eng |
| 内容記述 | A computer-aided engineering tool now in use at NASA for systems engineering and integration analysis of the Space Station is described. This tool, called IDEAS2, combines the spacecraft-specific analysis software from NASA IDEAS (truss synthesizer, rigid body controls, plume impingement, orbital lifetime, orbit heat loads, and life support systems) with the interactive graphics, geometric database, solids modeler, structural and thermal analysis capability of the SDRC I-DEAS to obtain an integrated package suitable for Space Station design. This integrated package was applied to a very recent study of growth scenarios of the Space Station dual keel configuration, in which a comparison was made between designs using a combination of photovoltaic solar arrays and solar dynamic collectors, and those using only solar dynamic collectors. |
| NASA分類 | SPACECRAFT DESIGN, TESTING AND PERFORMANCE |
| レポートNO | 86A38847
AIAA PAPER 86-0954 |
| 権利 | Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/384380 |
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