| タイトル | Preliminary weight and cost estimates for transport aircraft composite structural design concepts |
| 本文（外部サイト） | http://hdl.handle.net/2060/19730014249 |
| 著者所属（英） | General Dynamics/Fort Worth |
| 発行日 | 1973-03-30 |
| 言語 | eng |
| 内容記述 | Preliminary weight and cost estimates have been prepared for design concepts utilized for a transonic long range transport airframe with extensive applications of advanced composite materials. The design concepts, manufacturing approach, and anticipated details of manufacturing cost reflected in the composite airframe are substantially different from those found in conventional metal structure and offer further evidence of the advantages of advanced composite materials. |
| NASA分類 | AIRCRAFT |
| レポートNO | 73N22976
NASA-CR-112255 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/199326 |
