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Acta Armamentarii ›› 2023, Vol. 44 ›› Issue (4): 1097-1106.doi: 10.12382/bgxb.2021.0805

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Key Technology for Ultrasonic Measurement of Burning Rate in Large-scale Solid Rocket Motors

SUN Dechuan1,*(), XIAN Guang2   

  1. 1. School of Aeronautics and Astronautics, Dalian University of Technology, Dalian 116024, Liaoning, China
    2. The 41st Research Institute of No.6 Academy, China Aerospace Science & Industry Corporation, Hohhot 010010, Inner Mongolia, China
  • Received:2021-11-26 Online:2023-04-28
  • Contact: SUN Dechuan

Abstract:

Measuring the true burning rate of a solid rocket motor (SRM) is a challenging problem in SRM research and development. Ultrasonic measurement has been proven to be a feasible solution. This study provides an overview of the related technologies for measuring dynamic and large-scale motor burning rates using ultrasonic technology. Static tests of steel shell/propellant assembly and high-temperature verification tests of the steel shell solid motor are carried out using low-frequency ultrasonic technology. After review and experimental verification, it is determined that low-frequency ultrasonic is the most feasible approach for measuring the burning rate of large-scale SRM. A further research direction is to optimize the probe layout. The study also provides suggestions for ultrasonic data processing.

Key words: ultrasonic, burning rate, solid rocket motor