某弹载天线隔热设计仿真及试验验证  

Thermal Insulation Design Simulation and Experimental Verification of A Certain Missile-borne Antenna

作　　者：尤浩[1] YOU Hao(The 20th Research Institute of CETC,Xi’an 710068,China)

机构地区：[1]中国电子科技集团公司第二十研究所,陕西西安710068

出　　处：《舰船电子对抗》2021年第3期124-126,共3页Shipboard Electronic Countermeasure

摘　　要：超音速导弹产生的气动热对天线罩隔热能力有越来越高的要求。对某弹载天线的天线罩进行了隔热仿真分析,并设计了实物的验证试验,结果表明该天线罩可以保证天线的隔热需求。The aerodynamic heat generated by supersonic missile requires the heat insulation ability of radome higher and higher.This paper simulates and analyzes the thermal insulation of a certain missile-borne antenna radome,and design the verification test of real object.The results show that the radome can ensure the heat insulation requirement of the antenna.

关 键 词：耐高温 天线罩 热仿真分析 试验验证 

分 类 号：TK124[动力工程及工程热物理—工程热物理]