科技报告详细信息
| Heatshield for Extreme Entry Environment Technology (HEEET) Development and Maturation Status | |
| Ellerby, D ; Boghozian, T ; Driver, D ; Chavez-Garcia, J ; Fowler, M ; Gage, P ; Gasch, M ; Gonzales, G ; Kazemba, C ; Kellermann, C(NASA Johnson Space Center, Houston, TX, United States) | |
| 关键词: THERMAL PROTECTION; HEAT SHIELDING; ATMOSPHERIC ENTRY; ENVIRONMENTAL TESTS; LOAD TESTS; THERMAL ANALYSIS; STRUCTURAL ANALYSIS; SEAMS (JOINTS); TECHNOLOGY ASSESSMENT; WOVEN COMPOSITES; THICKNESS; SPACE ENVIRONMENT SIMULATION; SATURN (PLANET); VENUS (PLANET); GRAND TOURS; FINITE ELEMENT METHOD; | |
| RP-ID : ARC-E-DAA-TN52838 | |
| 学科分类:航空航天科学 | |
| 美国|英语 | |
| 来源: NASA Technical Reports Server | |
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【 摘 要 】
This poster provides an overview of the requirements, design, development and testing of the 3D (Three Dimensional) Woven TPS (Thermal Protection System) being developed under NASA's Heatshield for Extreme Entry Environment Technology (HEEET) project. Under this current program, NASA is working to develop a TPS capable of surviving entry into 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.
【 预 览 】
| Files | Size | Format | View |
|---|---|---|---|
| 20180001478.pdf | 5222KB |
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