BURNING CHARACTERISTICS OF COMPOSITE SOLID PROPELLANTS AT HIGH PRESSURES

被引：0

|

作者：

HAFF, C

GARNER, E

机构：

来源：

JOURNAL OF SPACECRAFT AND ROCKETS | 1969年 / 6卷 / 10期

关键词：

D O I：

暂无

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：1204 / &

相关论文

共 50 条

[41] MODEL OF EROSIVE BURNING OF COMPOSITE PROPELLANTS
KING, MK
JOURNAL OF SPACECRAFT AND ROCKETS, 1978, 15 (03) : 139 - 146
[42] Burning rate characteristics and ignition characteristics of ammonium nitrate/ammonium perchlorate composite propellants
1600, Japan Explosives Society, Tokyo, Japan (56):
[43] BURNING RATE MEASUREMENT OF SOLID PROPELLANTS
SPENADEL, L
REVIEW OF SCIENTIFIC INSTRUMENTS, 1961, 32 (07): : 837 - &
[44] THE THEORY OF BURNING OF SOLID AND LIQUID PROPELLANTS
SPALDING, DB
COMBUSTION AND FLAME, 1960, 4 (01) : 59 - 76
[45] EROSIVE BURNING OF SOLID-PROPELLANTS
KING, MK
JOURNAL OF PROPULSION AND POWER, 1993, 9 (06) : 785 - 805
[46] THEORETICAL INVESTIGATION IN STEADY STATE AND EROSIVE BURNING OF SOLID COMPOSITE PROPELLANTS.
Pei, Ming
Wang, Shoufan
Binggong Xuebao/Acta Armamentarii, 1988, (02): : 24 - 30
[47] PRESSURE-DEPENDENCE OF BURNING RATE OF COMPOSITE SOLID-PROPELLANTS - COMMENT
NELSON, CW
ADAMS, GF
WARD, JR
AIAA JOURNAL, 1979, 17 (02) : 222 - 223
[48] Tailoring burning rates using reactive wires in composite solid rocket propellants
Isert, Sarah
Lane, Colin D.
Gunduz, I. Emre
Son, Steven F.
PROCEEDINGS OF THE COMBUSTION INSTITUTE, 2017, 36 (02) : 2283 - 2290
[49] BURNING RATE PREDICTION OF COMPOSITE SOLID-PROPELLANTS USING FRACTAL GEOMETRY
MARVASTI, MA
STRAHLE, WC
COMBUSTION SCIENCE AND TECHNOLOGY, 1992, 83 (4-6) : 291 - 304
[50] PRESSURE-DEPENDENCE OF BURNING RATE OF COMPOSITE SOLID-PROPELLANTS - REPLY
RASTOGI, RP
SINGH, HJ
SRIVASTAVA, AK
AIAA JOURNAL, 1979, 17 (02) : 223 - 224

← 1 2 3 4 5 →