| タイトル | Advanced supersonic propulsion study, phase 4 |
| 本文（外部サイト） | http://hdl.handle.net/2060/19780003119 |
| 著者（英） | Howlett, R. A. |
| 著者所属（英） | Pratt and Whitney Aircraft Group |
| 発行日 | 1977-09-01 |
| 言語 | eng |
| 内容記述 | Installation characteristics for a Variable Stream Control Engine (VSCE) were studied for three advanced supersonic airplane designs. Sensitivity of the VSCE concept to change in technology projections was evaluated in terms of impact on overall installed performance. Based on these sensitivity results, critical technology requirements were reviewed, resulting in the reaffirmation of the following requirements: low-noise nozzle system; a high performance, low emissions duct burner and main burner; hot section technology; variable geometry components; and propulsion integration features, including an integrated electronic control system. |
| NASA分類 | AIRCRAFT PROPULSION AND POWER |
| レポートNO | 78N11062
PWA-5547-4
NASA-CR-135273 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/180712 |
