大展弦比巡飞弹挂固定翼载机投放研究  

Studies on Releasing High-Aspect Ratio Loitering Munition Suspended on Fixed Wing Aircraft

作　　者：韩果 丘杭海 朱鹏 罗敏芳 Han Guo;Qiu Hanghai;Zhu Peng;Luo Minfang(AVIC Hongdu,Nanchang,Jangxi,330024)

机构地区：[1]航空工业洪都,江西南昌330024

出　　处：《教练机》2024年第3期37-41,共5页Trainer

摘　　要：大展弦比巡飞弹由于其长航时的优势,在近年的局部冲突中越来越多地得以使用。巡飞弹由固定翼载机挂载投放是其重要的作战方式,由于速度差别,在投放过程中可能面临分离安全问题。本文分析了大展弦比巡飞弹挂固定翼载机投放时减速过程的特性,对基于减速伞的常规减速方式、基于发射筒/减速伞组合的减速方式及弹翼分阶段展开的变构型滑翔减速方式进行仿真分析,为机载巡飞弹投放方式设计提供了思路。Due to its advantage of long endurance,high aspect ratio loitering munition has been increasingly used in local conflicts in recent years.Suspending and releasing loitering munition on fixed wing aircraft is an important combat method,and due to differences in speed,there may be separation safety concerns during the releasing process.This article analyzes the characteristics of the deceleration process during the release of high aspect ratio loitering munition on a fixed wing aircraft.Simulation analysis has been conducted on the conventional deceleration method based on the drag chute,the deceleration method based on the combination of the missile launcher/drag chute,and the variable configuration gliding deceleration method with the wing unfolding in stages so as to provide thoughts for the design on releasing methods of airborne loitering munition.

关 键 词：巡飞弹 载机投放 减速伞 滑翔减速 

分 类 号：E932[兵器科学与技术—火炮、自动武器与弹药工程]