INVESTIGATION OF AN ADDITIONAL OXIDIZER CHARGE EFFECT ON SELECTED OPERATIONAL CHARACTERISTICS OF A SOLID-FUEL ROCKET ENGINE

被引：0
|
作者：
Zyluk, Andrzej [1 ]
Pietraszek, Mariusz [1 ]
机构：
[1] AF Inst Technol, Warsaw, Poland
来源：
JOURNAL OF THEORETICAL AND APPLIED MECHANICS | 2014年 / 52卷 / 01期
关键词：
oxygen balance; rocket engine; aircraft; experimental examination; oxidizer charge;
D O I：
暂无
中图分类号：
O3 [力学];
学科分类号：
08 ; 0801 ;
摘要：
The paper has been intended to discuss some issues closely related to the elimination of an extremely disadvantageous phenomenon, i.e. the occurrence of a negative oxygen balance in products of combustion emitted by a solid-fuel rocket engine while launching a missile from the aircraft. Findings of experimental examination of such engines furnished with an additional oxidizer charge have also been presented.
引用
收藏
页码：139 / 149
页数：11
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