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Optical detection of combustion zone movement in solid high-energy materials

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Combustion, Explosion, and Shock Waves Aims and scope

Abstract

Optical methods in infrared (IR) and visible (VIS) ranges for detection of combustion zone propagation in solid high-energy materials, such as pyrotechnic compositions inserted into pyrolytic graphite (pyrographite) tubes and ignited at one end by a CO2 laser beam are presented. The pyrographite tube is used as a thermal management transducer enabling detection of combustion zone movement because of unique thermal conductivity anisotropy of pyrographite resulting in low thermal conductivity of the tube along its axis and high thermal conductivity along the tube radius. In the first method, an IR thermal camera is applied for detection of heat zone movement induced on the external side surface of the pyrographite tube by the combustion zone travelling inside the tube. According to the second method, a VIS camera and a thermochromic layer covering the external side surface of the pyrographite tube are used for visualization of heat zone movement registered as the color change boundary traveling along the thermochromic layer. The change in color of this layer is caused by its thermochromic substance response to heat delivered by the heat zone. As thermochromic substances, leuko dyes or chiral-nematic liquid crystals are used. These methods seem to be particularly promising for continuous measurements of burning rates of solid high-energy materials, such as solid rocket propellants and pyrotechnic compositions.

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References

  1. G. G. Shelukhin, V. F. Buldakov, and V. P. Belov, “Experimental Study of Combustion of Condensed Systems,” Fiz. Goreniya Vzryva 5(1), 42–51 (1969).

    Google Scholar 

  2. Yu. V. Rozhdestvenskii, “Method and Technique of Studying Combustion Processes in Rocket Engines,” in Rocket Propellants, Ed. by Ya. M. Paushkin and A. Z. Chulkov (Mir, Moscow, 1975), pp. 171–187 [Russian translation].

    Google Scholar 

  3. V. A. Arkhipov, S. S. Bondarchuk, and A. G. Korotkikh, “Comparative Analysis of Methods for Measuring the Transient Burning Rate. I. Research Methods,” Fiz. Goreniya Vzryva 46(5), 82–87 (2010) [Combust., Explos., Shock Waves 46 (5), 564–569 (2010)].

    Google Scholar 

  4. V. A. Arkhipov, S. S. Bondarchuk, and A. G. Korotkikh, “Comparative Analysis of Methods for Measuring the Transient Burning Rate. II. Research Results,” Fiz. Goreniya Vzryva 46(5), 88–96 (2010) [Combust., Explos., Shock Waves 46 (5), 570–577 (2010)].

    Google Scholar 

  5. N. Eisenreich, H. P. Kugler, and F. Sinn, “An Optical System for Measuring the Burning Rate of Solid Propellant Strands,” Propel., Explos., Pyrotech. 12(2), 78–80 (1987).

    Article  ADS  Google Scholar 

  6. M. Miszczak, A. Panas, and W. Swiderski, “A New Method for Continuous Measurements of Solid Rocket Propellant Burning Rate with Use of IR Camera,” Measurement, Automation Monitoring 55(11), 950–953 (2009).

    Google Scholar 

  7. W. Swiderski and M. Miszczak, “A Novel Technique for the Continuous Evaluation of Burning Rate of Solid Rocket Propellant by Using IR Thermography,” QIRT J. 8(1), 111–114 (2011).

    Article  Google Scholar 

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Correspondence to W. Swiderski.

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Original Russian Text © M. Miszczak, W. Swiderski.

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Translated from Fizika Goreniya i Vzryva, Vol. 50, No. 2, pp. 62–67, March–April, 2014.

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Miszczak, M., Swiderski, W. Optical detection of combustion zone movement in solid high-energy materials. Combust Explos Shock Waves 50, 178–182 (2014). https://doi.org/10.1134/S0010508214020087

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  • DOI: https://doi.org/10.1134/S0010508214020087

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