Research progress of electrically controlled solid propulsion technology

被引：0
|
作者：
Wu J. [1 ]
Hu Z. [1 ]
He Z. [1 ]
Zhang Y. [1 ]
Ou Y. [1 ]
Ma Z. [1 ]
Peng Q. [1 ]
Zhong Y. [1 ]
机构：
[1] College of Aerospace Science, National University of Defense Technology, Changsha
来源：
Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica | 2023年 / 44卷 / 15期
基金：
中国国家自然科学基金;
关键词：
controllable solid propulsion; decomposition characteristics; electrically controlled solid propellant; igni⁃ tion combustion characteristics; solid micro-thruster; solid rocket motor;
D O I：
10.7527/S1000-6893.2023.28716
中图分类号：
学科分类号：
摘要：
Electrically controlled solid propulsion technology，including propellant-related technology and engine tech⁃ nology，realizes repeated engine start and real-time adjustable thrust by using a new type of propellant with electrically controlled combustion. With the advantages of being simple and reliable，this thrust adjustment method has a wide range of applications in the field of power systems for missile weapons and satellites. However，electrically controlled solid propellants are not mature enough，and various formulation systems need to be further optimized. Although elec⁃ trically controlled solid engines have been verified，there is still a large distance between the engine performance and actual application requirements. This paper comprehensively compares the technologies related with the electrically controlled solid propulsion，summarizes the latest research results in the field of this technology，and finally predicts the future development of electrically controlled solid propulsion technology，so as to provide some reference for the subsequent research. © 2023 AAAS Press of Chinese Society of Aeronautics and Astronautics. All rights reserved.
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