| タイトル | Vacuum plasma spray applications on liquid fuel rocket engines |
| 著者（英） | Bryant, M. A.; Zimmerman, F. R.; Mckechnie, T. N. |
| 著者所属（英） | NASA Marshall Space Flight Center |
| 発行日 | 1992-07-01 |
| 言語 | eng |
| 内容記述 | The vacuum plasma spray process (VPS) has been developed by NASA and Rocketdyne for a variety of applications on liquid fuel rocket engines, including the Space Shuttle Main Engine. These applications encompass thermal barrier coatings which are thermal shock resistant for turbopump blades and nozzles; bond coatings for cryogenic titanium components; wear resistant coatings and materials; high conductivity copper, NaRloy-Z, combustion chamber liners, and structural nickel base material, Inconel 718, for nozzle and combustion chamber support jackets. |
| NASA分類 | MECHANICAL ENGINEERING |
| レポートNO | 92A49051
AIAA PAPER 92-3527 |
| 権利 | Copyright |
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