| タイトル | Ares I-X Flight Test Vehicle:Stack 1 Modal Test |
| 本文（外部サイト） | http://hdl.handle.net/2060/20100011898 |
| 著者（英） | Gaspar, James L.; Horta, Lucas G.; Lazor, Daniel R.; Bartolotta, Paul A.; Reaves, Mercedes C.; Templeton, Justin D.; Parks, Russel A.; Buehrle, Ralph D. |
| 著者所属（英） | NASA Langley Research Center |
| 発行日 | 2010-03-01 |
| 言語 | eng |
| 内容記述 | Ares I-X was the first flight test vehicle used in the development of NASA s Ares I crew launch vehicle. The Ares I-X used a 4-segment reusable solid rocket booster from the Space Shuttle heritage with mass simulators for the 5th segment, upper stage, crew module and launch abort system. Three modal tests were defined to verify the dynamic finite element model of the Ares I-X flight test vehicle. Test configurations included two partial stacks and the full Ares I-X flight test vehicle on the Mobile Launcher Platform. This report focuses on the second modal test that was performed on the middle section of the vehicle referred to as Stack 1, which consisted of the subassembly from the 5th segment simulator through the interstage. This report describes the test requirements, constraints, pre-test analysis, test operations and data analysis for the Ares I-X Stack 1 modal test. |
| NASA分類 | Spacecraft Design, Testing and Performance |
| レポートNO | L-19840
NASA/TM-2010-216210
LF99-10302 |
| 権利 | No Copyright |
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