Correlation between the chemical composition, heat content, and specific impulse of solid propellants optimized in terms of energy

被引:0
|
作者
Lempert, DB [1 ]
Nechiporenko, GN [1 ]
Dolganova, GP [1 ]
机构
[1] Russian Acad Sci, Inst Problems Chem Phys, Chernogolovka 142432, Moscow Region, Russia
来源
CHEMICAL PHYSICS REPORTS | 1998年 / 17卷 / 07期
关键词
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中图分类号
O64 [物理化学(理论化学)、化学物理学]; O56 [分子物理学、原子物理学];
学科分类号
070203 ; 070304 ; 081704 ; 1406 ;
摘要
The dependence of the specific impulse of solid propellants on their total heat content and chemical composition is studied. The conditions and quantitative criteria needed to optimize the propellant composition in terms of energy are determined; an algorithm and user computer program for predicting optimized compositions with a preset specific impulse value that offer an opportunity of constructing one of the propellant components from molecular fragments suggested.
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页码:1333 / 1342
页数:10
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