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高超声速飞行器空基拦截方案设计

刘双喜 刘伟 闫斌斌 黄伟 闫杰

航空兵器2024,Vol.31Issue(1):32-37,6.
航空兵器2024,Vol.31Issue(1):32-37,6.DOI:10.12132/ISSN.1673-5048.2023.0174

高超声速飞行器空基拦截方案设计

Design of Air-Based Interception Scheme for Hypersonic Vehicles

刘双喜 1刘伟 2闫斌斌 3黄伟 1闫杰4

作者信息

  • 1. 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
  • 2. 上海航天设备制造总厂有限公司,上海 200245
  • 3. 西北工业大学 航天学院,西安 710072
  • 4. 西北工业大学 无人系统技术研究院,西安 710072
  • 折叠

摘要

Abstract

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.

关键词

高超声速飞行器/空基拦截/空天防御/临近空间

Key words

hypersonic vehicle/air-based interception/air and space defense/near-space

分类

军事科技

引用本文复制引用

刘双喜,刘伟,闫斌斌,黄伟,闫杰..高超声速飞行器空基拦截方案设计[J].航空兵器,2024,31(1):32-37,6.

基金项目

航空科学基金项目(20200001053005) (20200001053005)

湖南省杰出青年基金项目(2021JJ10045) (2021JJ10045)

智能博弈重点实验室创新工作站开放课题(ZBKF-24-01) (ZBKF-24-01)

航空兵器

OA北大核心CSTPCD

1673-5048

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