| タイトル | Aerodynamic characteristics of two single-stage-to-orbit vehicles at Mach 20.3 |
| 本文（外部サイト） | http://hdl.handle.net/2060/19770022265 |
| 著者（英） | Bernot, P. T. |
| 著者所属（英） | NASA Langley Research Center |
| 発行日 | 1977-08-01 |
| 言語 | eng |
| 内容記述 | The hypersonic stability, control, and performance characteristics of two configurations have been determined. Each configuration had a 50 deg swept delta wing, a vertical tail, and a body flap. One model represented a control configured vehicle with a reduced level of longitudinal static stability; the other model was designed for a conventional level of stability. Data were obtained over an angle of attack range of 0 deg to 50 deg and included effects of component buildup. In addition, the effects of the vertical tail on the lateral directional characteristics were obtained. |
| NASA分類 | SPACE TRANSPORTATION |
| レポートNO | 77N29209
NASA-TM-X-3550
L-11627 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/181548 |
