| タイトル | Static stability and control effectiveness of models 12-0 and 34-0 of the vehicle 3 configuration, volume 3 |
| 本文（外部サイト） | http://hdl.handle.net/2060/19740004405 |
| 著者（英） | Allen, E. C.; Tuttle, T. |
| 著者所属（英） | Chrysler Corp. |
| 発行日 | 1973-10-01 |
| 言語 | eng |
| 内容記述 | Static stability and control effectiveness characteristics of two 0.004 scale models of the vehicle 3 configuration are reported. The components investigated consisted of a single aft body, vertical/rudder, OMS pods with two interchangeable wings, four interchangeable forward bodies, four trimmers, and a spoiler. The test was conducted in 14 x 14 inch trisonic wind tunnel over a Mach number range from 0.6 to 4.96. Angles of attack from 0 to 60 degrees and angles of sideslip from -10 to 10 degrees at 0, 10, 20,30, and 40 degrees angle of attack were tested. Elevon, body flap, and speed brake deflection composed the parametric considerations. No grit was placed on the models during the test. The tabulated source data and incremental data figures are presented. |
| NASA分類 | SPACE VEHICLES |
| レポートNO | 74N12518
DMS-DR-2055-VOL-3
NASA-CR-128780-VOL-3 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/196593 |
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