Compatibility of injector materials with hydrogen peroxide propellant

被引：0
|
作者：
Gostowski, R [1 ]
机构：
[1] NASA, George C Marshall Space Flight Ctr, Prop Res Ctr, Huntsville, AL 35812 USA
来源：
JOURNAL OF PROPULSION AND POWER | 2004年 / 20卷 / 06期
关键词：
D O I：
10.2514/1.7092
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
Compatibility evaluation of rocket grade hydrogen peroxide (RGHP) was discussed. RGHP is hydrogen peroxide in concentrations ranging from 85 to 98% with a defined aerospace set of additives. RGHP is considered to have much less toxicity than other monopropellants and oxidizers. It was found that isothermal microcalorimeter provides a simple, reproducible, and sensitive means to assess quantitatively compatibility of injector materials with RGHP propellant.
引用
收藏
页码：1126 / 1127
页数：2
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