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Energy Characteristic of Nitramine HTPB Propellant Containing RDX as Oxidizer
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    Abstract:

    In order to investigate the energy property of RDX/AP/Al/HTPB propellant, theoretical calculation is conducted. By the ignition experiment of BSF 165 mm and BSF 315 mm motor,We summarize the regularity of energy property with the change of RDX content in propellant and chamber pressure of motor. The optimum formulating is designed according to the results of theoretical calculation and experiment.The comparative tests by 760 mm motor have further confirmed the contribution of RDX in specific impulse, and the actual specific impulse is 2 428.1 N·s·kg-1(pc=6.86 MPa) of 760 mm motor.

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袁桂芳,胡建军,赵文胜,等.含RDX的硝胺丁羟推进剂能量特性研究[J].含能材料,2002,10(4):157-160.
YUAN Gui-fang, HU Jian-jun, ZHAO Wen-sheng, et al. Energy Characteristic of Nitramine HTPB Propellant Containing RDX as Oxidizer[J]. Chinese Journal of Energetic Materials,2002,10(4):157-160.

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History
  • Received:May 17,2002
  • Revised:
  • Adopted:
  • Online: November 03,2011
  • Published: