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A Study of Propellant with Low Erosion and High Combustion Progressivity
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Xi’an Modern Chemistry Research Institute

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    Abstract:

    The modified single base propellant was prepared by using an impregnated-deterred technology. The erosion of the propellant to barrel was characterized by erosion tube test. The static combustion performances of the propellant were investigated by closed-bomb test. The dynamic interior ballistic performance of the propellant was studied by 857-30 mm gun. The results show that compared with the conventional single propellant,the barrel erosion of the modified single base propellant decreases by 16.4%,the value of progression factor (Pr) increases from 0.035 to 0.445,and the muzzle velocity increases by 9.8% from 856.6 m·s-1 to 941.3 m·s-1,revealing that the modified single propellant prepared in this work has the advantages of high combustion progressivity and low erosion.

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刘波,王琼林,刘少武,等.一种低烧蚀高渐增性发射药的研究[J].含能材料,2011,19(5):565-568.
LIU Bo, WANG Qiong-lin, LIU Shao-wu, et al. A Study of Propellant with Low Erosion and High Combustion Progressivity[J]. Chinese Journal of Energetic Materials,2011,19(5):565-568.

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History
  • Received:January 26,2011
  • Revised:May 23,2011
  • Adopted:March 25,2011
  • Online: February 22,2012
  • Published: