Finite element analysis of propellant of solid rocket motor during ship motion

Abstract

In order to simulate the stress and strain of solid rocket motors (SRMs), a finite element analysis model was established. The stress spectra of the SRM elements with respect to time in the case that the vessel cruises under a certain shipping condition were obtained by simulation. According to the analysis of the simulation results, a critical zone was confirmed, and the Mises stress amplitudes of the different critical zones were acquired. The results show that the maximum stress and strain of SRM are less than the maximum tensile strength and elongation, respectively, of the propellant. The cumulative damage of the motor must also be evaluated by random fatigue loading.

Keywords

• Shipborne missile
• Solid rocket motor
• Propellant
• Finite element analysis
• Mises stress