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A Viscoelastic Constitutive Model of Propellant with Pressure Cure

Cui, ZX; Li, HY; Shen, ZB; Cui, HR

Shen, ZB (corresponding author), Natl Univ Def Technol, Coll Aerosp Sci & Engn, Changsha 410073, Peoples R China.; Shen, ZB (corresponding author), Hunan Key Lab Intelligent Planning & Simulat Aero, Changsha 410073, Peoples R China.

PROPELLANTS EXPLOSIVES PYROTECHNICS, 2021; 46 (7): 1036

Abstract

The application of pressure cure molding technology can effectively reduce the structural integrity problems of casting solid rocket motors. In order ......

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