COMBUSTION WAVE STRUCTURES OF AMMONIUM-PERCHLORATE COMPOSITE PROPELLANTS

被引:17
作者
KUBOTA, N
KUWAHARA, T
MIYAZAKI, S
UCHIYAMA, K
HIRATA, N
机构
[1] NISSAN MOTOR CO LTD,DIV AERONAUT & SPACE,SUGINAMI,TOKYO,JAPAN
[2] NIPPON OIL & FATS CO LTD,DIV SOLID PROPELLANT RES,TAKETOYO PLANT,TAKETOYO,AICHI,JAPAN
[3] DAICEL CHEM IND LTD,DIV SOLID PROPELLANT RES,HARIMA PLANT,HYOGO,JAPAN
关键词
D O I
10.2514/3.22885
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
10
引用
收藏
页码:296 / 300
页数:5
相关论文
共 11 条
[1]  
BASTRESS EK, 1961, THESIS PRINCETON U P
[2]  
Beckstead MW., 1970, AIAA J, V8, P2200, DOI [10.2514/3.6087, DOI 10.2514/3.6087]
[3]   CONTRIBUTION OF SOLID-PHASE HEAT RELEASE TO AP COMPOSITE-PROPELLANT BURNING RATE [J].
CAVENY, LH ;
PITTMAN, CU .
AIAA JOURNAL, 1968, 6 (08) :1461-&
[4]   A MODEL OF COMPOSITE PROPELLANT COMBUSTION INCLUDING SURFACE HETEROGENEITY AND HEAT GENERATION [J].
HERMANCE, CE .
AIAA JOURNAL, 1966, 4 (09) :1629-+
[5]  
HILL WE, 1976, ADA035404
[6]  
KUBOTA N, 1982, 19TH S INT COMB PITT, P777
[7]  
KUBOTA N, 1981, AIAA811582 PAP
[8]   COMBUSTION OF RDX AP COMPOSITE PROPELLANTS AT LOW-PRESSURES [J].
KUWAHARA, T ;
KUBOTA, N .
JOURNAL OF SPACECRAFT AND ROCKETS, 1984, 21 (05) :502-507
[9]  
KUWAHARA T, UNPUB COMBUSTION SCI
[10]   MEASUREMENT OF TEMPERATURE PROFILES THROUGH SOLID-PROPELLANT FLAMES USING FINE THERMOCOUPLES [J].
SABADELL, AJ ;
WENOGRAD, J ;
SUMMERFI.M .
AIAA JOURNAL, 1965, 3 (09) :1580-&