| 一种新型环形发动机装药设计 |
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| 引用本文： | 王春利.一种新型环形发动机装药设计[J].推进技术,1996,17(2):66-70. |
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| 作者姓名： | 王春利 |
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| 作者单位： | 北京理工大学飞行器工程系 |
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| 摘 要： | 根据某反坦克导弹动力装置的要求，设计了一种新型环形发动机装药，称为异型管状药柱。这种装药具有短时间工作提供大推力的特点，介绍了该药形的设计方法。
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| 关 键 词： | 固体推进剂火箭发动要机，环形发动机，发射药装药结构，计算机辅助设计 |
PROPELLANT DESIGN FOR A NEW TYPE OF ANNULAR ROCKET MOTORS |
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| Wang Chunli.PROPELLANT DESIGN FOR A NEW TYPE OF ANNULAR ROCKET MOTORS[J].Journal of Propulsion Technology,1996,17(2):66-70. |
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| Authors: | Wang Chunli |
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| Institution: | Depe. of Flight Vehicle Engineering, Beijing Inst. of Technology, Beijing, 100081 |
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| Abstract: | n accordance with propelling equipments design requirements of a long range anti-tank missile, a propellant configuration, named irregular-tube-form charge, used for a new type of annular rocket motors is designed. This kind of propellant is characterized by big propelling force and short working time. The design method of this propellant configuration is introduced in this paper. |
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| Keywords: | Solid propellant rocket engine Annular engine Propellant charge structure Computer aided design |
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