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Temperature Coefficient of the Modified Single-based Propellant
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Xi’an Modern Chemistry Research Institute

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    Abstract:

    The modified single-based propellant was prepared by the "impregnated-deterred-coated" technology.The combustion and interior ballistic performances of the propellant were investigated by closed-bomb and 857-30 mm gun.The structure of the modified single-based propellant was analyzed.The results show that in comparison with conventional single-based propellant, the muzzle velocity of modified single-based propellant increases by 5% at least at normal, high and low temperatures.The modified single-based propellant has the characteristics of low temperature coefficient when used in the 857-30 mm gun.It is resulted from the formation of the zipper structure with end sealing and the softness of the body surface.

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刘少武,刘波,王琼林,等.改性单基发射药温度系数研究[J].含能材料,2012,20(3):345-348.
LIU Shao-wu, LIU Bo, WANG Qiong-lin, et al. Temperature Coefficient of the Modified Single-based Propellant[J]. Chinese Journal of Energetic Materials,2012,20(3):345-348.

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History
  • Received:May 13,2011
  • Revised:December 03,2011
  • Adopted:December 30,2011
  • Online: June 01,2012
  • Published: