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HTPB-based polyurethanes for inhibition of composite propellants

โœ Scribed by D. C. Gupta; S. S. Deo; D. V. Wast; S. S. Raomore; D. H. Gholap


Publisher
John Wiley and Sons
Year
1995
Tongue
English
Weight
391 KB
Volume
55
Category
Article
ISSN
0021-8995

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Polyurethanes were synthesized by the reaction of hydroxy-terminated polybutadiene (HTPB) and diisocyanates such as toluene diisocyanate (TDI), diphenylmethane diisocyanate (MDI), hexamethylene diisocyanate (HMDI), and isophorone diisocyanate (IPDI). Carbon black and antimonytrioxide (Sb 2 O 3 ) wer

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## Abstract Composite propellants based on hydroxylโ€terminated polybutadience (HTPB) resin are the most common contemporary solid propellants for launch vehicle and missile applications. A series of HTPB resins, manufactured by freeโ€radical polymerisation using a peroxide initiator, with varying mo

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Aging behavior of hydroxyl-terminated polybutadiene/ammonium perchlorate (HTPB/AP)-based composite solid propellants was studied as a function of crosslink density, which is predominantly determined by the molar ratio of diisocyanate to total hydroxyl (NCO/OH ratio) and the molar ratio of triol to d