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A survey on ceramic radome failure types and the importance of defect determination

天线罩 导弹 灾难性故障 结构工程 工程类 陶瓷 材料科学 航空航天工程 天线(收音机) 复合材料 电气工程
作者
Şeyma Saliha Fidan,Rahmi Ünal
出处
期刊:Engineering Failure Analysis [Elsevier]
卷期号:149: 107234-107234
标识
DOI:10.1016/j.engfailanal.2023.107234
摘要

A missile is a tube-shaped air vehicle that travels long distances through the air and has a radio frequency seeker that exchanges signal with radar against possible threats. A structure called a radome is placed on the missile nose, and it protects the seeker antenna from the external environment. The radome material must have electromagnetic permeability, high thermal shock resistance, and a certain level of strength to maintain its integrity under flight conditions. Ceramic materials with the optimum combination of these properties are preferred as missile radome materials. Ceramic radomes are also expected to be erosion-resistant and maintain their structural stability along with the thermal and structural loads. Since the increasing competition conditions require reaching higher missile speeds (Ma > 5) today, a radome is needed to develop resistant to these speeds. Under harsh flight loads on the radome can cause severe damage that may lead to fracture. This review study discusses the literature on radome failure types, the effects of structural defects on radome failure, and the importance of defect determination. It is found that thermal and mechanical loads can cause catastrophic fractures at the connection point of the radome with the missile body, which is the most critical failure type. Detecting structural defects like micro cracks is vital for high-quality radome production. The number of micro-cracks formed during the production of radomes increases with an increase in part size. For this reason, coupon tests are insufficient to detect the behavior of large-volume parts. Consequently, statistical methods such as the Weibull distribution determine the damage-based radome behavior. Another critical issue for a radome is to verify its structural integrity, and ground tests should be applied to prevent possible failure during flight tests. In conclusion, this review provides researchers with a general and future perspective about possible failure types, defect detection methods, and ground test systems for ceramic radome.
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