装备环境工程
裝備環境工程
장비배경공정
EQUIPMENT ENVIRONMENTAL ENGINEERING
2015年
2期
99-103
,共5页
空空导弹%高低温%工作温度
空空導彈%高低溫%工作溫度
공공도탄%고저온%공작온도
air-to-air missile%high and low temperature%operating temperature
目的：分析空空导弹高低温工作温度的考核要求。方法基于空空导弹的特点，给出其寿命期内预期经历的高低温工作环境，并对在这些环境下遭遇的极端温度进行分析。结果以空空导弹挂装某两型载机为例，综合考虑了寿命期内各阶段工作环境，给出了高低温工作温度的确定方法以及考核建议。结论由于各型号空空导弹的部署区域和挂装载机不同，文中提供的高低温工作温度参考值并不能覆盖所有型号的空空导弹，仍需具体问题具体分析，以获得相对准确的工作温度，对其环境适应性做出合理评价。
目的：分析空空導彈高低溫工作溫度的攷覈要求。方法基于空空導彈的特點，給齣其壽命期內預期經歷的高低溫工作環境，併對在這些環境下遭遇的極耑溫度進行分析。結果以空空導彈掛裝某兩型載機為例，綜閤攷慮瞭壽命期內各階段工作環境，給齣瞭高低溫工作溫度的確定方法以及攷覈建議。結論由于各型號空空導彈的部署區域和掛裝載機不同，文中提供的高低溫工作溫度參攷值併不能覆蓋所有型號的空空導彈，仍需具體問題具體分析，以穫得相對準確的工作溫度，對其環境適應性做齣閤理評價。
목적：분석공공도탄고저온공작온도적고핵요구。방법기우공공도탄적특점，급출기수명기내예기경력적고저온공작배경，병대재저사배경하조우적겁단온도진행분석。결과이공공도탄괘장모량형재궤위례，종합고필료수명기내각계단공작배경，급출료고저온공작온도적학정방법이급고핵건의。결론유우각형호공공도탄적부서구역화괘장재궤불동，문중제공적고저온공작온도삼고치병불능복개소유형호적공공도탄，잉수구체문제구체분석，이획득상대준학적공작온도，대기배경괄응성주출합리평개。
Objective To analyze the assessment requirements of high and low operating temperature for air-to-air missiles. Methods Based on the characteristics of air-to-air missile, the expected high and low operating environments throughout its life cycle were given, and the extreme temperatures under these environments were analyzed. Results A two-type carrier aircraft with air-to-air missile was taken as an example, the operating environments at different stages of the life cycle were comprehensively considered and the determination method as well as assessment suggestions for high and low operating temperature were given. Conclusion As different air-to-air missiles have different deployment area and carrier aircraft, the reference values of high and low operating temperature given in this paper could not cover all types of air-to-air missiles, so we should make a concrete analysis of each specific question to obtain relatively accurate operating temperature and to reasonably judge the environmental adaptability.
