| タイトル | Rotary-Wing Decelerators for Probe Descent Through the Atmosphere of Venus |
| 本文（外部サイト） | http://hdl.handle.net/2060/20070014645 |
| 著者（英） | Briggs, Geoffrey; Young, Larry A.; Pisanich, Greg; Aiken, Edwin |
| 著者所属（英） | NASA Ames Research Center |
| 発行日 | 2005-04-01 |
| 言語 | eng |
| 内容記述 | An innovative concept is proposed for atmospheric entry probe deceleration, wherein one or more deployed rotors (in autorotation or wind-turbine flow states) on the aft end of the probe effect controlled descent. This concept is particularly oriented toward probes intended to land safely on the surface of Venus. Initial work on design trade studies is discussed. |
| NASA分類 | Space Sciences (General) |
| 権利 | Copyright, Distribution as joint owner in the copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/564949 |
