| タイトル | Arc Jet Results on Candidate High Temperature Coatings for NASA's NGLT Refractory Composite Leading Edge Task |
| 本文（外部サイト） | http://hdl.handle.net/2060/20040040337 |
| 著者（英） | Vaughn, W. L.; Lewis, R. K.; Milhoan, J. D.; Ohlhorst, C. W. |
| 著者所属（英） | NASA Langley Research Center |
| 発行日 | 2004-01-16 |
| 言語 | eng |
| 内容記述 | In 2000, arc jet testing was conducted on thirteen material systems for possible use on the nose leading edge of the Hyper-X program s X-43A Mach 10 vehicle. Six material systems survived 3, 130- second cycles. To support NASA s Next Generation Launch Technology Programs (NGLT) need for passive refractory composite leading edges with multiple reuse capability at temperatures up to 3600 F, these six materials were subjected to an expanded arc jet test program. This expanded arc jet test program included three phases. The purpose of the first phase was to generate emissivity data as a function of temperature. The purpose of the second phase was to determine if the material systems had any thermal cycling durability, and the third phase was to determine whether the materials could survive an arc jet test of one hour duration. Some of the coating systems were found to have very low emissivities, suggesting that they would not be good candidates for leading edges coating. Other coating systems survived both the second and third phases of the test program and showed potential for use as an oxidation protection coating for leading edges. This presentation summarizes the test program results. |
| NASA分類 | Metals and Metallic Materials |
| 権利 | No Copyright |
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