| タイトル | Aerothermal Ground Testing of Flexible Thermal Protection Systems for Hypersonic Inflatable Aerodynamic Decelerators |
| 本文（外部サイト） | http://hdl.handle.net/2060/20120011663 |
| 著者（英） | Bruce, Walter E., III; Tobin, Steven A.; Kardell, Matthew P.; Siemers, Paul M., III; DelCorso, Joseph A.; Ferlemann, Paul G.; Hughes, Stephen J.; Mesick, Nathaniel J. |
| 著者所属（英） | NASA Langley Research Center |
| 発行日 | 2012-06-18 |
| 言語 | eng |
| 内容記述 | Flexible TPS development involves ground testing and analysis necessary to characterize performance of the FTPS candidates prior to flight testing. This paper provides an overview of the analysis and ground testing efforts performed over the last year at the NASA Langley Research Center and in the Boeing Large-Core Arc Tunnel (LCAT). In the LCAT test series, material layups were subjected to aerothermal loads commensurate with peak re-entry conditions enveloping a range of HIAD mission trajectories. The FTPS layups were tested over a heat flux range from 20 to 50 W/cm with associated surface pressures of 3 to 8 kPa. To support the testing effort a significant redesign of the existing shear (wedge) model holder from previous testing efforts was undertaken to develop a new test technique for supporting and evaluating the FTPS in the high-temperature, arc jet flow. Since the FTPS test samples typically experience a geometry change during testing, computational fluid dynamic (CFD) models of the arc jet flow field and test model were developed to support the testing effort. The CFD results were used to help determine the test conditions experienced by the test samples as the surface geometry changes. This paper includes an overview of the Boeing LCAT facility, the general approach for testing FTPS, CFD analysis methodology and results, model holder design and test methodology, and selected thermal results of several FTPS layups. |
| NASA分類 | Spacecraft Design, Testing and Performance |
| レポートNO | NF1676L-14924 |
| 権利 | Copyright, Distribution as joint owner in the copyright |
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