タイトル | System automatically provides dynamic launch decision criteria |
本文(外部サイト) | http://hdl.handle.net/2060/19670000363 |
著者(英) | Doig, J. E. |
発行日 | 1967-10-01 |
言語 | eng |
内容記述 | Saturn 5 Dynamic Launch Decision Criteria model provides instantaneous criteria, derived from the parametric behavior of a complex system such as a space launch vehicle plus its payload, for the decision making of launch management personnel. |
NASA分類 | ELECTRONIC COMPONENTS AND CIRCUITS |
レポートNO | 67B10363 MFS-13063 |
権利 | No Copyright |
URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/503810 |