HTPB-BASED POLYURETHANES FOR INHIBITION OF COMPOSITE PROPELLANTS

被引:13
作者
GUPTA, DC [1 ]
DEO, SS [1 ]
WAST, DV [1 ]
RAOMORE, SS [1 ]
GHOLAP, DH [1 ]
机构
[1] EXPLOS RES & DEV LAB,POONA 411008,MAHARASHTRA,INDIA
关键词
D O I
10.1002/app.1995.070550801
中图分类号
O63 [高分子化学(高聚物)];
学科分类号
070305 ; 080501 ; 081704 ;
摘要
Polyurethanes were synthesized by the reaction of hydroxyterminated polybutadiene (HTPB) and diisocyanates such as toluene diisocyanate (TDI), diphenylmethane diisocyanate (MDI), hexamethylene diisocyanate (HMDI), and isophoron diisocyanate (IPDI). A number of fillers such as carbon black, kaolin, and antimony trioxide (Sb2O3) were used in these formulations. Mechanical and thermal stability of these polyurethanes were studied. Based on its properties, HTPB-MDI derived filled polyurethane was selected and evaluated as an inhibitor for a composite propellant. (C) 1995 John Wiley and Sons, Inc.
引用
收藏
页码:1151 / 1155
页数:5
相关论文
共 24 条
[1]  
AGRAWAL JP, 1991, COMPOS MANUF, V2, P48
[2]  
AGRAWAL JP, 1993, PROPELL EXPLOS PYROT, V18, P155
[3]  
ALLEN HC, 1980, Patent No. 4209351
[4]  
[Anonymous], 1980, U.S. Pat., Patent No. [4 187 215, 4187215]
[5]  
BUIST JM, 1970, ADV POLYURETHANE TEC, P195
[6]  
CLIFFORD DV, 1976, Patent No. 1448087
[8]  
FUST GW, 1966, APPL POLYM S, V4, P222
[9]  
HUMPHRIES J, 1956, ROCKET GUIDED MISSIL, V33
[10]  
KARAJU K, 1992, HIGH ENERGY MAT SOC