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QIU Shuang, SU Yingli, YANG Haitao. Influence of propellant composition on performance of solid fuel ramjet[J]. Journal of Aerospace Power, 2020, 35(9): 1995-2005. doi: 10.13224/j.cnki.jasp.2020.09.022
Citation: QIU Shuang, SU Yingli, YANG Haitao. Influence of propellant composition on performance of solid fuel ramjet[J]. Journal of Aerospace Power, 2020, 35(9): 1995-2005. doi: 10.13224/j.cnki.jasp.2020.09.022
shu

Influence of propellant composition on performance of solid fuel ramjet

doi: 10.13224/j.cnki.jasp.2020.09.022
  • 1.

    School of Mechanical Engineering,Nanjing University of Science and Technology,Nanjing 210094,China

  • 2.

    Shanghai Aircraft Design and Research Institute,Commercial Aircraft Corporation of China Limited,Shanghai 201210,China

  • 3.

    System Engineering Institute of Sichuan Aerospace,China Aerospace Science and Technology Corporation,Chengdu 610100,China

  • Received Date: 2020-03-03
  • Publish Date: 2020-09-28
    Abstract
  • In order to investigate the influence of different component propellants on the performance of solid fuel ramjet(SFRJ), experiments were conducted on connected pipe facility for ignition of a SFRJ using polyethylene(PE) with paraffin, carbon black and carbon fiber as propellant. The combustion surface morphology was observed by SEM. The three-dimensional distribution of regression rate was obtained by using three-dimensional scanner and data reconstruction method. According to the data obtained from the experiment, the performance parameters of SFRJ under different working conditions were further calculated. Results indicated that: addition of 5% Carbon fiber could hinder the mechanical erosion of combustion surface of the polyethylene-based propellant and affect the pyrolysis process, making it impossible for self-sustaining combustion. The Kelvin-Helmholtz instability was found through the three-dimensional distribution of burning rate. Adding carbon black and paraffin to the polyethylene-based propellant could improve the regression rate, and the influence of paraffin was more obvious. The mass fraction of paraffin of 30%, 50% paraffin and pure paraffin were 375%, 514% and 544% higher than those of PE respectively. Finally, the relationship between the average regression rate of the polyethylene-based propellant and the mass fraction of paraffin was obtained.

     

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