膏体推进剂点火和燃烧特性的实验研究  

An experimental study on the ignition and combustion characteristics of pasty propellant

作　　者：张明信[1] 张胜勇[1] 

机构地区：[1]中国航天科技集团公司四院四十一所,西安710025

出　　处：《固体火箭技术》2003年第2期30-32,共3页Journal of Solid Rocket Technology

摘　　要：膏体推进剂的点火和燃烧特性是发动机设计的重要参数。本实验研究给出的PEPA/AP膏体推进剂自燃温度约为150℃,容易点燃;在工作压强大于0.6MPa时的燃烧临界直径小于1mm。在发动机工作状态下的燃速与静态燃速一致。预计该推进剂适合于多次起动的发动机。The ignition and combustion characteristics of pasty propellant are important parameters for the motor design. An experimental study on the pasty propellant named PEPA/AP was carried out. The results show that the autoignition temperature of this propellant is about 150℃, so it is easy to ignite. As the chamber pressure is greater than 0.6MPa, the critical combustion diameter is less than 1mm. As the test motor is in operation, its propellant burning rate accords with the static burning rate. It is predicted that the propellant will be suitable for multiplestart motor.

关 键 词：膏体推进剂 点火 燃烧特性 实验研究 发动机 固体推进剂 

分 类 号：V435[航空宇航科学与技术—航空宇航推进理论与工程] V512