Investigation of fuel-rich boron combustion in a pressurized combustion bomb

被引：0
|
作者：
Pein, R [1 ]
Anders, S [1 ]
机构：
[1] DLR, Geman Aerosp Ctr, D-74239 Hardthausen, Germany
来源：
COMBUSTION OF ENERGETIC MATERIALS | 2002年
关键词：
ducted rocket; boron combustion;
D O I：
暂无
中图分类号：
O414.1 [热力学];
学科分类号：
摘要：
Small pellets of two different fuel-rich boron propellants were burnt in a pressurized combustion bomb in order to investigate the combustion in ducted rocket primary combustion chambers. The pressure varied between 1 and 100 bar. The combustion products were chemically analyzed for boron, boron oxide, and boron carbide. The results were plotted versus pressure and compared with computed equilibrium compositions. The main conclusion is that considerable extent of boron conversion into reaction products is already taking place in the primary gas generator of a ducted rocket.
引用
收藏
页码：427 / 437
页数：5
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