航天推进技术研究院主办
[1]马 帅,郭健鑫,周 磊,等.固体火箭发动机技术发展综述[J].火箭推进,2023,49(02):1-14.
MA Shuai,GUO Jianxin,ZHOU Lei,et al.Review on technology development of solid rocket motor[J].Journal of Rocket Propulsion,2023,49(02):1-14.
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MA Shuai,GUO Jianxin,ZHOU Lei,et al.Review on technology development of solid rocket motor[J].Journal of Rocket Propulsion,2023,49(02):1-14.
固体火箭发动机技术发展综述
《火箭推进》[ISSN:1672-9374/CN:CN 61-1436/V]
卷:
49
期数:
2023年02期
页码:
1-14
栏目:
目次
出版日期:
2023-04-25
- Title:
- Review on technology development of solid rocket motor
- 文章编号:
- 1672-9374(2023)02-0001-14
- Keywords:
- solid rocket motor; booster; missile; single pulse; dual pulse; propellant; attitude control
- 分类号:
- V435
- 文献标志码:
- A
- 摘要:
- 火箭发动机的研制始终是推进航天技术和探索未知空间的重要支柱,固体火箭发动机以成本低、可靠性高等特点,常被选作推进系统,针对航天工程中火箭运载、在轨维修和精确制导等技术的需求,重点梳理了多年来美国、俄国、日本、欧洲和中国固体火箭发动机的研究进展与成果。以火箭运载和精确制导为临界点,将固体火箭发动机进行大小型区分,基于整体式和分段式的特点,列表对比了大型固体火箭发动机的长度、直径、推力等重要技术参数。沿着时间的发展主线,概述了小型单/双脉冲固体火箭发动机的工作原理、结构参数、飞行测试结果等。通过对比国内外的研究成果,揭示了国内固体火箭发动机发展的技术差距,提出了固体火箭发动机发展的关键技术。
- Abstract:
- The development of rocket motor has always been an important pillar to promote aerospace technology and explore unknown space.Solid rocket motor is often selected as the propulsion system because of its low cost and high reliability.In view of the requirements of rocket launch, on-orbit maintenance and precision guidance in aerospace engineering, the research progress and achievements of solid rocket motor including the United States, Russia, Japan, Europe and China over the years have been emphatically summarized.Taking the rocket launch and precise guidance as the critical point, solid rocket motor is divided into large and small.Based on the characteristics of integral and segmented, the important technical parameters such as length, diameter and thrust of large solid rocket motor are listed and compared.Along the main line of time development, the working principle, structural parameters and flight test results of small single/dual pulse solid rocket motor are summarized.Through the comparison of this research, the technical gap in the development of domestic solid rocket motor is revealed, and the key technologies are put forward.
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备注/Memo
收稿日期:2022-01-25; 修回日期:2022-04-02
基金项目:国家自然科学基金资助项目(51605026)
作者简介:马帅(1995—),男,硕士,助理工程师,研究领域为航空航天发动机试车台设计及发动机试验、测试技术。
更新日期/Last Update:
1900-01-01