UDMH／N2O4爆炸冲击波特性研究

推进技术 ›› 1996, Vol. 17 ›› Issue (4): 77-81.

UDMH／N₂O₄爆炸冲击波特性研究

鄢小清,王振国,黎勤武,刘昆

国防科技大学航天技术系;国防科技大学航天技术系;国防科技大学航天技术系;国防科技大学航天技术系

发布日期:2021-08-15

A STUDY ON BLAST CHARACTERISTICS OF UDMH/N₂O₄ PROPELLANT EXPLOSIONS

Dept. of Aerospace Technology, National Univ.of Defense Technology, Changsha, 410073;Dept. of Aerospace Technology, National Univ.of Defense Technology, Changsha, 410073;Dept. of Aerospace Technology, National Univ.of Defense Technology, Changsha, 410073;Dept. of Aerospace Technology, National Univ.of Defense Technology, Changsha, 410073

Published:2021-08-15

摘要/Abstract

摘要： 研究了ＵＤＭＨ／Ｎ２Ｏ４爆炸冲击波的一般机理和规律，引进了ＴＮＴ等价重量、极限当量两个基本概念，建立了三种爆炸模式，从理论上对爆炸冲击波特性进行了计算，确立了各种冲击波特性参数的分布规律。计算结果与国外有关资料进行了比较，数据基本吻合，并针对１０ｋｇ、５０ｋｇ、１００ｋｇ、３００ｋｇ实验进行了计算和比较。

关键词: 液体火箭推进剂;推进剂爆炸;冲击波参数;测试技术

Abstract: The general mechanism and rules of blast characteristics of UDMH/N2O4 propellantexplosions are studied. Two essential concepts, TNT equivalent weight and terminal yield, are adopted. Three explosion modes are established. Blast characteristics of UDMH/N2O4 propellant explosionsare calculated with the theory we developed, and the parameters of distributing rules of blast characteristics of explosions are established. Compared with references abroad, reasonably good correlationis achieved. Blast characteristics of 10 kg, 50 kg, 100 kg and 300 kg UDMH/N2O4 propellant explosions are calculated and compared with the experiment data.

Key words: Liquid rocket propellant;Propellant explosion;Shock wave parameter;Measuring technique

鄢小清,王振国,黎勤武,刘昆. UDMH／N₂O₄爆炸冲击波特性研究[J]. 推进技术, 1996, 17(4): 77-81.

UDMH／N₂O₄爆炸冲击波特性研究

A STUDY ON BLAST CHARACTERISTICS OF UDMH/N₂O₄ PROPELLANT EXPLOSIONS

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