固体燃料火箭
组分(热力学)
可靠性(半导体)
火箭(武器)
火箭发动机
可靠性工程
汽车工程
损害赔偿
工程类
太空发射
系统工程
航空航天工程
机械工程
法律工程学
运载火箭
推进剂
功率(物理)
法学
物理
热力学
量子力学
政治学
作者
Dipesh Dhital,Jung‐Ryul Lee,Charles R. Farrar,David Mascareñas
标识
DOI:10.1177/1045389x13493360
摘要
Rocket engines are complex systems which usually operate under extreme physical conditions such as very high temperature and pressure, strong erosion, and high-density energy release. Mechanical and chemical complexity, long service lives, aging materials, and designs with small margins of safety are typical for space launch vehicle components including the engine. Furthermore, these components can be exposed to various flaws and damage during the manufacturing, assembly, or ground handling phase. In regard to the engine, its performance characteristics can be significantly affected by the degradation resulting from such flaws and damages, which, in turn, might lead to failure of the entire space mission. Any manufacturing/operational damage needs to be detected at the earliest stage possible, so that the required preventive measures can be implemented, and component readiness and reliability must be checked either during manufacturing or during field inspections. This review study lists such possible flaws/damages on rocket engine components. This information could be beneficial for determining and developing the efficient techniques for reliable nondestructive evaluation and structural health monitoring.
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