| タイトル | Study of hypersonic propulsion/airframe integration technology |
| 本文（外部サイト） | http://hdl.handle.net/2060/19780011153 |
| 著者（英） | Goebel, T. P.; Vancamp, V. V.; Hartill, W. R. |
| 著者所属（英） | Rockwell International Corp. |
| 発行日 | 1978-01-01 |
| 言語 | eng |
| 内容記述 | An assessment is done of current and potential ground facilities, and analysis and flight test techniques for establishing a hypersonic propulsion/airframe integration technology base. A mach 6 cruise prototype aircraft incorporating integrated Scramjet engines was considered the baseline configuration, and the assessment focused on the aerodynamic and configuration aspects of the integration technology. The study describes the key technology milestones that must be met to permit a decision on development of a prototype vehicle, and defines risk levels for these milestones. Capabilities and limitations of analysis techniques, current and potential ground test facilities, and flight test techniques are described in terms of the milestones and risk levels. |
| NASA分類 | AIRCRAFT DESIGN, TESTING AND PERFORMANCE |
| レポートNO | 78N19096
NASA-CR-145321
NA-78-24 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/179667 |
