| タイトル | The X-43A Hyper-X Mach 7 Flight 2 Guidance, Navigation, and Control Overview and Flight Test Results |
| 本文（外部サイト） | http://hdl.handle.net/2060/20050182778 |
| 著者（英） | Bahm, Catherine; Martin, John; Beck, Roger E.; Bose, David; Baumann, Ethan; Strovers, Brian |
| 著者所属（英） | NASA Dryden Flight Research Center |
| 発行日 | 2005-01-01 |
| 言語 | eng |
| 内容記述 | The objective of the Hyper-X program was to flight demonstrate an airframe-integrated hypersonic vehicle. On March 27, 2004, the Hyper-X program team successfully conducted flight 2 and achieved all of the research objectives. The Hyper-X research vehicle successfully separated from the Hyper-X launch vehicle and achieved the desired engine test conditions before the experiment began. The research vehicle rejected the disturbances caused by the cowl door opening and the fuel turning on and off and maintained the engine test conditions throughout the experiment. After the engine test was complete, the vehicle recovered and descended along a trajectory while performing research maneuvers. The last data acquired showed that the vehicle maintained control to the water. This report will provide an overview of the research vehicle guidance and control systems and the performance of the vehicle during the separation event and engine test. The research maneuvers were performed to collect data for aerodynamics and flight controls research. This report also will provide an overview of the flight controls related research and results. |
| NASA分類 | Ground Support Systems and Facilities (Space) |
| 権利 | Copyright, Distribution as joint owner in the copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/219990 |
