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高超声速飞行器空基拦截方案设计OA北大核心CSTPCD

Design of Air-Based Interception Scheme for Hypersonic Vehicles

中文摘要英文摘要

高超声速飞行器防御作战对于各国都是一个巨大的挑战,相关研究方案仍处于论证阶段,具体的作战方式尚未形成统一认知.针对临近空间高超声速飞行器防御问题,本文基于典型防空反导体系的设计过程,在合理作战想定的基础上开展了高超声速飞行器空基拦截方案设计工作.首先,阐述了高超声速飞行器五大性能优势.然后,分析了高超声速飞行器典型弹道特性和空基拦截的优势.最后,从系统组成、作战流程和作战时序三个方面对高超声速飞行器空基拦截方案进行描述.

The defense of hypersonic vehicles in combat poses a significant challenge for all countries.However,the related research is still in the demonstration stage and there is no unified understanding of specific combat methods.In response to the defense problem of hypersonic vehicles in near-space,this paper presents a design process for the defense against near-space hypersonic vehicles based on a typical anti-air defense missile system.The design work of air-based interception schemes for hypersonic vehicles is conducted on the basis of reasonable combat scenarios.Firstly,it describes the five major performance advantages of hypersonic vehicles.Then,it analyzes the typical trajectory characteristics of hypersonic vehicles and the advantages of air-based in-terception.Finally,it describes the air-based interception scheme of hypersonic vehicles from three aspects:system composition,operational process,and operational timing,which provides a reference for future near-space defense system construction.

刘双喜;刘伟;闫斌斌;黄伟;闫杰

国防科技大学 空天科学学院,长沙 410073||国防科技大学 高超声速技术实验室,长沙 410073上海航天设备制造总厂有限公司,上海 200245西北工业大学 航天学院,西安 710072西北工业大学 无人系统技术研究院,西安 710072

武器工业

高超声速飞行器空基拦截空天防御临近空间

hypersonic vehicleair-based interceptionair and space defensenear-space

《航空兵器》 2024 (001)

32-37 / 6

航空科学基金项目(20200001053005);湖南省杰出青年基金项目(2021JJ10045);智能博弈重点实验室创新工作站开放课题(ZBKF-24-01)

10.12132/ISSN.1673-5048.2023.0174

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