IMPROVED COMPOSITE SOLID PROPELLANTS INCLUDING A HYDROXY-FUNCTIONAL POLYBUTADIENE BINDER AND A ROCKET MOTOR INCLUDING SAME

摘要

Solid propellants for rocket motors contain binders which are hydroxy-functional polybutadiene (HFPB). The HFPB is difunctional and the diene linkages are exclusively 1,4-diene linkages, with no vinyl groups. A rocket motor may contain the solid propellant.