| タイトル | Heatshield for Extreme Entry Environment Technology (HEEET) Enabling Missions Beyond Heritage Carbon Phenolic |
| 本文（外部サイト） | http://hdl.handle.net/2060/20150007678 |
| 著者（英） | Gonzaes, G.; Fowler, M.; Ellerby, D.; Boghozian, T.; Hamm, K.; Chinnapongse, R.; Stackpoole, M.; Chavez-Garcia, J.; Blosser, M.; Peterson, K.; Beerman, A.; Kazemba, C.; Gasch, M.; Nishioka, O.; Milos, F.; Young, Z.; Mahzari, M.; Poteet, C.; Prabhu, D.; Gage, P.; Ma, J.; Splinter, S.; Venkatapathy, E. |
| 著者所属（英） | NASA Ames Research Center |
| 発行日 | 2015-04-09 |
| 言語 | eng |
| 内容記述 | This poster provides an overview of the requirements, design, development and testing of the 3D Woven TPS being developed under NASAs Heatshield for Extreme Entry Environment Technology (HEEET) project. Under this current program, NASA is working to develop a Thermal Protection System (TPS) capable of surviving entry into Venus or Saturn. A primary goal of the project is to build and test an Engineering Test Unit (ETU) to establish a Technical Readiness Level (TRL) of 6 for this technology by 2017. |
| NASA分類 | Fluid Mechanics and Thermodynamics; Structural Mechanics; Astrodynamics; Spacecraft Design, Testing and Performance |
| レポートNO | ARC-E-DAA-TN22184 |
| 権利 | Copyright, Distribution as joint owner in the copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/562297 |
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