IGNITION AND SURFACE TEMPERATURES OF DOUBLE BASE PROPELLANTS AT LOW PRESSURES .2. COMPARISON OF OPTICAL AND THERMOCOUPLE TECHNIQUES

被引:4
作者
ROGERS, CR
SUH, NP
机构
关键词
D O I
10.2514/3.5930
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:1501 / &
相关论文
共 22 条
[1]  
DATTA A, 1966, THESIS U SOUTH CAROL
[2]   EXPERIMENTAL TECHNIQUES FOR SOLID-PROPELLANT COMBUSTION RESEARCH [J].
FRIEDMAN, R .
AIAA JOURNAL, 1967, 5 (07) :1217-&
[3]  
HEATH GA, 1962, 8TH S INT COMB PITTS, P711
[4]  
HEATH GA, 1957, RPD161 TN ROYAL AIRC
[5]   STRUCTURE OF THE GAS PHASE COMBUSTION REGION OF A SOLID DOUBLE BASE PROPELLANT [J].
HELLER, CA ;
GORDON, AS .
JOURNAL OF PHYSICAL CHEMISTRY, 1955, 59 (08) :773-777
[6]  
JAMES NE, 1964, 1964 REVIEW RESEARCH, P183
[7]  
KIRBY CE, 1970, AIAA70125 PAP
[8]   DETERMINATION OF THE THERMAL STRUCTURE OF A COMBUSTION WAVE BY FINE THERMOCOUPLES [J].
KLEIN, R ;
MENTSER, M ;
VONELBE, G ;
LEWIS, B .
JOURNAL OF PHYSICAL AND COLLOID CHEMISTRY, 1950, 54 (06) :877-884
[9]  
MICHELI P, 1968, 109081F AER GEN CORP
[10]  
MICHELI PL, 1968, CR66487 NASA