| タイトル | IRVE-3 Post-Flight Reconstruction |
| 本文（外部サイト） | http://hdl.handle.net/2060/20130013398 |
| 著者（英） | Bowden, Ernest; Lindell, Michael; Olds, Aaron D.; Hollis, Brian; Gsell, Valerie; Bose, David; White, Joseph; Cheatwood, F. N.; Edquist, Karl; Beck, Roger |
| 著者所属（英） | NASA Langley Research Center |
| 発行日 | 2013-03-25 |
| 言語 | eng |
| 内容記述 | The Inflatable Re-entry Vehicle Experiment 3 (IRVE-3) was conducted from the NASA Wallops Flight Facility on July 23, 2012. Launched on a Black Brant XI sounding rocket, the IRVE-3 research vehicle achieved an apogee of 469 km, deployed and inflated a Hypersonic Inflatable Aerodynamic Decelerator (HIAD), re-entered the Earth's atmosphere at Mach 10 and achieved a peak deceleration of 20 g's before descending to splashdown roughly 20 minutes after launch. This paper presents the filtering methodology and results associated with the development of the Best Estimated Trajectory of the IRVE-3 flight test. The reconstructed trajectory is compared against project requirements and pre-flight predictions of entry state, aerodynamics, HIAD flexibility, and attitude control system performance. |
| NASA分類 | Spacecraft Design, Testing and Performance |
| レポートNO | AIAA Paper 1514242 |
| 権利 | Copyright, Distribution as joint owner in the copyright |
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