Development of modern solid propellants

被引:125
作者
Davenas, A [1 ]
机构
[1] SNPE, F-75004 Paris, France
关键词
D O I
10.2514/2.6947
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:1108 / 1128
页数:21
相关论文
共 181 条
[1]  
*AGARD, 1997, 350 AGARD ADV
[2]  
*AGARD, 1993, AGARD LECT SER, V188
[3]  
ANDREPONT WC, 1994, 943057 AIAA
[4]  
[Anonymous], 1984, FUNDAMENTALS SOLID P
[5]  
[Anonymous], 1975, PHYS RUBBER ELASTICI
[6]  
[Anonymous], 1993, SOLID ROCKET PROPULS, DOI DOI 10.1016/13978-0-08-010999-3.50011
[7]  
[Anonymous], 983981 AIAA
[8]  
AOKIN I, 1994, 943059 AIAA
[9]  
Arendale W. F., 1969, PROPELLANTS MANUFACT, V88, P67
[10]   Burning rate of solid propellant ingredients, Part 2: Determination of burning rate temperature sensitivity [J].
Atwood, AI ;
Boggs, TL ;
Curran, PO ;
Parr, TP ;
Hanson-Parr, DM ;
Price, CF ;
Wiknich, J .
JOURNAL OF PROPULSION AND POWER, 1999, 15 (06) :748-752