双基推进剂压力响应函数的实验研究

推进技术 ›› 1992, Vol. 13 ›› Issue (6): 81-84.

双基推进剂压力响应函数的实验研究

王宁飞,赵崇信,张暹,王秀维,孙维申

西安近代化学研究所;西安近代化学研究所;西安近代化学研究所;西安近代化学研究所;西安近代化学研究所

发布日期:2021-08-15

EXPERIMENTAL RESEARCH ON THE PRESSURE-COUPLING RESPONSE OF DOUBLE-BASE PROPELLANT

Xian Modern Chemistry Research Institute;Xian Modern Chemistry Research Institute;Xian Modern Chemistry Research Institute;Xian Modern Chemistry Research Institute;Xian Modern Chemistry Research Institute

Published:2021-08-15

摘要/Abstract

摘要： 讨论了可控式T型燃烧器测量推进剂压力耦合响应函数的原理及方法,列出三种双基推进剂在各种温度、频率和压力下的测量结果。

关键词: 固体火箭发动机;双基推进剂;燃烧振动;燃烧稳定性

Abstract: The authors have discussed the principle and method of determining pressure-coupling response function of propellants with the controllable T-burner, and presented the results of three double-base propellants in high initial temperature, normal initial temperature and low initial temperature at various frequences and various pressures.

Key words: Solid rocket engine;Double-base propellant;Combustion vibration;Combustion stability

王宁飞,赵崇信,张暹,王秀维,孙维申. 双基推进剂压力响应函数的实验研究[J]. 推进技术, 1992, 13(6): 81-84.