TENSILE STRAIN-RATE EFFECT IN MECHANICAL-PROPERTIES OF DUMMY HTPB PROPELLANTS

被引:16
作者
CHUNG, HL
KAWATA, K
ITABASHI, M
机构
[1] Department of Materials Science and Technology, Faculty of Industrial Science and Technology, Science University of Tokyo, Noda, Chiba
关键词
Polybutadienes;
D O I
10.1002/app.1993.070500108
中图分类号
O63 [高分子化学(高聚物)];
学科分类号
070305 ; 080501 ; 081704 ;
摘要
The tensile strain rate effect in tensile strength and elongation at break for a series of filled dummy hydroxy-terminated polybutadiene (HTPB) propellant binders was studied. The data were obtained at various tensile strain rates from 10(-4) to 10(-1) s-1 on two types of specimens at room temperature. The ''high velocity ductility'' behavior, which is qualitatively similar to those of unfilled elastomers, was revealed. This means that the breaking strain increases markedly at elevated strain rates. For ''Bukkon-type'' and rod-shaped specimens, test results are consistent with each other. The fact that the increased filled solids level leads to a decreased breaking elongation capability and an increased tensile strength was obviously found. (C) 1993 John Wiley & Sons, Inc.
引用
收藏
页码:57 / 66
页数:10
相关论文
共 17 条
[1]   RELATION OF MECHANICAL PROPERTIES TO SOLID ROCKET MOTOR FAILURE [J].
BILLS, KW ;
WIEGAND, JH .
AIAA JOURNAL, 1963, 1 (09) :2116-2123
[2]  
KAWATA K, 1969, B I SPACE AERON SCI, V5, P521
[3]  
KAWATA K, 1993, 6TH P JAP US C COMP, P771
[4]  
KAWATA K, 1989, 19TH P AIRCR AER MAT, P51
[5]  
KAWATA K, 1969, B I SPACE AERON SCI, V5, P506
[6]   VISCOELASTIC PROPERTIES OF RUBBERLIKE COMPOSITE PROPELLANTS AND FILLED ELASTOMERS [J].
LANDEL, RF ;
SMITH, TL .
ARS JOURNAL, 1961, 31 (05) :599-608
[7]  
LANDEL RF, 1958, CBS66 CIT JET PROP L
[8]  
MILLOWAY WT, 1963, J APPL POLYM SCI, V7, P1325
[9]  
NAGAPPA R, 1990, AIAA902331 PAP
[10]  
RAJAN M, 1975, AIAA751344 PAP