| タイトル | Design definition study of NASA/Navy lift/cruise fan V/STOL aircraft |
| 本文（外部サイト） | http://hdl.handle.net/2060/19760011018 |
| 著者所属（英） | Rockwell International Corp. |
| 発行日 | 1975-09-01 |
| 言語 | eng |
| 内容記述 | Assessed are the risks associated with the lift/cruise fan technology V/STOL aircraft program. Three candidate concepts for the technology aircraft design approach are considered: the lowspeed only modification, the full performance modification, and the all new aircraft concepts. Survey results indicate that the lift/cruise fan technology aircraft program is feasible, from the standpoint of technical risk, with some evidence of uncertainty of meeting the planned schedule and relatively minor impact on estimated program costs. |
| NASA分類 | AIRCRAFT DESIGN, TESTING AND PERFORMANCE |
| レポートNO | 76N18106
NASA-CR-137727 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/187017 |
