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Acta Armamentarii ›› 2022, Vol. 43 ›› Issue (3): 489-502.doi: 10.12382/bgxb.2021.0136

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Motion Trajectory of Solid Particles in C1xb Solid Rocket Motor

GU Xingpeng1, LI Junwei1, QIAO Wensheng2, WU Sheng2, HAN Lei1, WANG Qi1, WANG Ningfei1   

  1. (1.School of Aerospace Engineering,Beijing Institute of Technology,Beijing 100081,China;2.Inner Mongolia Power Machinery Research Institute,Hohhot 010010,Inner Mongolia,China)
  • Online:2022-04-07

Abstract: The force of condensed-phase particles in C1xb solid rocket motor (SRM) is analyzed based on internal flow field of motor. The velocity and acceleration of particle at different moments are obtained,and a two-dimensional particle motion trajectory model is established. Based on this model,the spatial distribution rule of particles in SRM is obtained. On this basis,the effects of motor rotation,initial position of particle and particle size on the movement of condensed-phase particles are studied. Results show that the particles leaving the upstream and downstream surfaces of aluminized hydroxyl-terminated-polybutadiene propellant have a greater probability of colliding with inner wall. Larger size particles increase the probability of collision with inner wall during particle movement. Rotation has more influence on spatial distribution of particles in motor in comparison with axial overload.

Key words: C1xbsolidrocketmotor, condensed-phaseparticle, forceonparticle, particlemotiontrajectory, particlesize

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