COMBUSTION OF RDX AP COMPOSITE PROPELLANTS AT LOW-PRESSURES

被引:14
作者
KUWAHARA, T [1 ]
KUBOTA, N [1 ]
机构
[1] JAPAN DEF AGCY,CTR RES 3,ROCKET PROPULS LAB,TOKYO,JAPAN
关键词
D O I
10.2514/3.25686
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
引用
收藏
页码:502 / 507
页数:6
相关论文
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