降低颗粒粘结高燃速推进剂初始压强峰的途径

推进技术 ›› 2004, Vol. 25 ›› Issue (1): 86-88.

降低颗粒粘结高燃速推进剂初始压强峰的途径

郭效德,张丽荣,李凤生

山西兴安化学材料厂;山西太原030008;山西兴安化学材料厂;山西太原030008;南京理工大学化工学院;江苏南京210094

发布日期:2021-08-15

Measures to reduce the initial pressure peak of grain binding high burning rate propellant

Shanxi Xing’an Chemical Materials Plant, Taiyuan 030008, China;Shanxi Xing’an Chemical Materials Plant, Taiyuan 030008, China;School of Chemical Engineering, Nanjing Univ. of Science and Technology, Nanjing 210094, China

Published:2021-08-15

摘要/Abstract

摘要： 为降低颗粒粘结高燃速推进剂发动机试验时的初始压强峰,分别采用降低点火药量,改变燃喉比、燃通比,内外表面涂钝感剂和控制内、外燃通比之比小于1等方法进行了发动机试验,获得了每种条件下的压峰比数据。分析结果表明,采用控制内、外燃通比之比小于1的装填条件,可使其高燃速推进剂的压峰比小于1 3。

关键词: 高燃速推进剂;颗粒;粘接;压力比

Abstract: In order to reduce the initial pressure peak of grain binding high burning rate propellant in motor test, the motor test was carried out based on the measures of reducing the quantity of igniter charge, the ratio of burning surface to throat area (K), the ratio of burning surface to port area (χ), coating phlegmatizer on the inner and outer surfaces and controlling the ratio of interal χ(in) to exteral χ(ex) within 1. The date of peak pressure ratio were also given. It shows that adopting the measure of controlling the ratio of interal χ(in) to exteral χ(ex) within 1 can make the peak pressure ratio of high burning rate propellant lower than 1.3 by analyzing the date.

Key words: High burning rate propellant;Particle;Bonding;Pressure ratio

郭效德,张丽荣,李凤生. 降低颗粒粘结高燃速推进剂初始压强峰的途径[J]. 推进技术, 2004, 25(1): 86-88.