A parallel evaluation test device for ablation performance of solid engine insulation layer
A solid engine, ablation test technology, applied in the direction of engine testing, jet engine testing, gas turbine engine testing, etc., can solve the ablation performance deviation of adiabatic materials, ablation environment fluctuations, unfavorable adiabatic material formula improvement design assessment Evaluation and other issues, to achieve the effect of reducing radial loss, convenient installation and use, and simple structure
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[0030]In this embodiment, a parallel test device for evaluating the ablation performance of a solid engine thermal insulation layer is machined and installed; among them, the front head mandrel 1, the combustion chamber front head 2, the combustion chamber barrel section 4, the combustion chamber rear head 10, the ablation The test section 11 and the nozzle holder 14 use 45 # The steel is processed and formed, and the sealing ring 8 is made of silicone rubber. The propellant 3 is a three-component butylated hydroxy propellant, which uses a cylindrical grain of end-face combustion, and the other surfaces are covered. The diameter of the grain is 200 mm, the length is 67.2 mm, and the thickness of the coating layer is 3 mm.
[0031] The length of the combustion chamber barrel section 4 is 180mm, the outer diameter is 230mm, and the inner diameter is 210mm. The flanges at both ends of the combustion chamber barrel section 4 have 12 holes uniformly opened along the circumference, ...
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