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What is Enhancing Mechanical Properties of Rocket Propellants about?

This document discusses improving the mechanical properties of composite rocket propellants. It aims to increase the tensile strength of hydroxyl-terminated polybutadiene (HTPB) and decrease the glass transition temperature of poly(3-nitratomethyl-3-methyl oxetane) (PolyNIMMO). The document provides background on the typical composition and manufacturing of solid composite rocket propellants. It also discusses the importance of mechanical properties and how properties like tensile strength and glass transit

Author

xcv

Language

EN