航空学报 > 2023, Vol. 44 Issue (23): 629555-629555   doi: 10.7527/S1000-6893.2023.29555

可重复使用运载火箭技术专栏

可重复使用运载火箭技术发展综述

包为民()   

  1. 中国航天科技集团有限公司,北京 100048
  • 收稿日期:2023-09-08 修回日期:2023-09-14 接受日期:2023-09-27 出版日期:2023-12-15 发布日期:2023-09-27
  • 通讯作者: 包为民 E-mail:baoweimin@cashq.ac.cn

A review of reusable launch vehicle technology development

Weimin BAO()   

  1. China Aerospace Science and Technology Corporation,Beijing 100048,China
  • Received:2023-09-08 Revised:2023-09-14 Accepted:2023-09-27 Online:2023-12-15 Published:2023-09-27
  • Contact: Weimin BAO E-mail:baoweimin@cashq.ac.cn

摘要:

可重复使用运载火箭是实现人类大规模低成本进出空间的重要途径。本文从垂直起降可重复使用运载火箭的技术需求出发,梳理了垂直起降可重复使用运载火箭面临的技术难题,并从技术难题分析得到垂直起降可重复使用运载火箭的关键技术。从总体优化设计、动力、结构与热防护、导航、制导与控制和健康管理等方面,对垂直起降可重复使用运载火箭关键技术的研究进展与未来发展方向进行了总结,可为可重复使用运载火箭的技术攻关提供参考。

关键词: 可重复使用运载火箭, 总体优化设计, 火箭发动机, 结构与热防护, 导航制导与控制, 运载火箭健康管理

Abstract:

Reusable launch vehicles are an important way for humans to enter and exit space on a large scale and at a low cost. Starting from the technical requirements of vertical takeoff and landing reusable launch vehicles, this paper summarizes the technical challenges faced by vertical takeoff and landing reusable launch vehicles, and analyzes the key technologies of vertical takeoff and landing reusable launch vehicles. The research progress and future development directions of key technologies for vertical takeoff and landing reusable launch vehicles are then discussed in terms of overall optimization design, power, structure and thermal protection, navigation, guidance and control, and health management, which can provide reference for the technical research of reusable launch vehicles.

Key words: reusable launch vehicle, system optimization design, rocket engine, structure and thermal protection, navigation guidance and control, launch vehicle health management

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