Rocket engine combustion chamber design concepts for enhanced life
摘要:
The lifetime of rocket combustion chambers can be increased by applying thermal barrier coatings. The standard coating systems usually used in gas turbines or aero engines will fail at the bond coat/substrate interface due to the chemical difference as well as the different thermal expansion between the copper liner and the applied NiCrAlY bond coat. A new bond coat alloy for rocket engine...
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会议名称:
32nd Joint Propulsion Conference and Exhibit
会议时间:
1996/07/22
被引量:
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