Interior Performances of an Impulse Thruster by Numerical Calculation |
| |
Authors: | YANG Qing WANG Li-qiong WANG Pei-lan HUANG Ge-de |
| |
Affiliation: | 1. State Key Laboratory of Explosion Science and Technology, Beijing Institute of Technology, Beijing 100081, China 2. China North Industries Corporation, Beijing 100053, China |
| |
Abstract: | Impulse thruster is a kind of actuator used for trajectory correction or attitude control of some in-flight munitions and vehicles.A simple mathematical model was set up to model interior characteristics of an impulse thruster.With this model,effects of some key parameters on interior performances of the impulse thruster were studied.Results show that action time is affected significantly by nozzle throat diameter and volume of combustion chamber,while output impulse is sensitive to charge particle diameter... |
| |
Keywords: | impulse thruster trajectory correction interior performances numerical calculation |
本文献已被 CNKI 维普 万方数据 等数据库收录! |
| 点击此处可从《北京理工大学学报(英文版)》浏览原始摘要信息 |
|
点击此处可从《北京理工大学学报(英文版)》下载全文 |