A CALORIMETRIC BOMB FOR DETERMINING HEATS OF COMBUSTION OF HYPERGOLIC PROPELLANTS

被引：2

作者：

JAIN, SR ^{[1
]}

RAJENDRAN, G ^{[1
]}

机构：

[1] INDIAN INST SCI,DEPT INORGAN & PHYS CHEM,BANGALORE 560012,KARNATAKA,INDIA

来源：

JOURNAL OF SPACECRAFT AND ROCKETS | 1986年 / 23卷 / 01期

关键词：

D O I：

10.2514/3.25795

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

引用

页码：120 / 122

页数：3

共 13 条

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[9] NOVEL SOLID HYPERGOLIC FUELS FOR HYBRID PROPELLANTS [J].

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[10] MECHANISM OF COMBUSTION OF LIQUID ROCKET PROPELLANTS - ALIPHATIC ALCOHOLS AND MIXED ACID [J].

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