Condensed combustion products at the burning surface of aluminized solid propellant

被引：89

作者：

Babuk, VA ^{[1
]}

Vasilyev, VA ^{[1
]}

Malakhov, MS ^{[1
]}

机构：

[1] Balt State Tech Univ, Dept Space Vehicles & Rocket Motors, St Petersburg 198005, Russia

来源：

JOURNAL OF PROPULSION AND POWER | 1999年 / 15卷 / 06期

关键词：

D O I：

10.2514/2.5497

中图分类号：

V [航空、航天];

学科分类号：

08 [工学]; 0825 [航空宇航科学与技术];

摘要：

Experimental results are presented on the formation of condensed combustion products (CCPs) at the burning surface of aluminized solid propellants. A number of experimental techniques were developed for describing the characteristics of the CCPs as a function of the oxidizer particle size and pressure. The results of this investigation provide qualitative descriptions of the CCPs formed at the propellant burning surface as functions of oxidizer particle size and pressure.

引用

页码：783 / 793

页数：11

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