| タイトル | Interactive systems design and synthesis of future spacecraft concepts |
| 本文（外部サイト） | http://hdl.handle.net/2060/19840020824 |
| 著者（英） | Wright, R. L.; Ferebee, M. J., Jr.; Deryder, D. D. |
| 著者所属（英） | NASA Langley Research Center |
| 発行日 | 1984-06-01 |
| 言語 | eng |
| 内容記述 | An interactive systems design and synthesis is performed on future spacecraft concepts using the Interactive Design and Evaluation of Advanced spacecraft (IDEAS) computer-aided design and analysis system. The capabilities and advantages of the systems-oriented interactive computer-aided design and analysis system are described. The synthesis of both large antenna and space station concepts, and space station evolutionary growth is demonstrated. The IDEAS program provides the user with both an interactive graphics and an interactive computing capability which consists of over 40 multidisciplinary synthesis and analysis modules. Thus, the user can create, analyze and conduct parametric studies and modify Earth-orbiting spacecraft designs (space stations, large antennas or platforms, and technologically advanced spacecraft) at an interactive terminal with relative ease. The IDEAS approach is useful during the conceptual design phase of advanced space missions when a multiplicity of parameters and concepts must be analyzed and evaluated in a cost-effective and timely manner. |
| NASA分類 | SPACECRAFT DESIGN, TESTING AND PERFORMANCE |
| レポートNO | 84N28893
NAS 1.15:86254
NASA-TM-86254 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/158937 |
