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整体级发动机用含硼BAMO/THF推进剂的探索研究 被引量:2

A PRIMARY STUDY ON BORON-CONTAINING BAMO/THF PROPELLANTS USED IN INTEGRATED STAGE MOTORS
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摘要 采用最小自由能法(white法),计算研究了增塑剂与粘合剂质量比(P1、P0)、固体含量、硼含量、HMX含量对用于整体级发动机的含硼BAMO/THF(1:1)推进剂能量的影响。实验研究制得的65%固体含量的BAMO/THF(1:1)含硼固体推进剂的基础燃速、压强指数较低;φ65mm发动机的试车结果表明:实验制得的65%固体含量的含硼BAMO/THF(1:1)推进剂的比冲效率为84.45%。 Based on the minimum free energy method (white method), the effects of mass ratio of plasticizer and polymer (P1/P0), solid loading, boron powder content and HMX content on the energetic characteristics of boron-containing BAMO/THF (1: 1) propellants, which will be used in integrated stage motors, have been studied by thermodynamic calculation. AP/B/ [BAMO/THF (1: 1 )] propellants with solid loading of 65% have been made, the sample has slower burning rate and lower pressure exponent. The test results of 65mm motor show that the specific impulse efficiency of the sample is 84. 45%.
作者 王锐鑫 苏峰
出处 《推进技术》 EI CAS CSCD 北大核心 1996年第6期87-90,共4页 Journal of Propulsion Technology
关键词 高能材料 推进剂配方 能量性能 Energetic material Boron Propellant formulation Energetic property
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  • 1于胜春,蔡体敏,何洪庆,张兆源,王思民.强制偏流喷管的实验研究[J].推进技术,1995,16(2):17-20. 被引量:4
  • 2关大林 王宁飞.改善硼粒子点火及燃烧性能研究的回顾与展望[J].火炸药学报,1998,(2):52-54.
  • 3王文俊.2000年固体推进剂的发展预测[J].固体火箭技术,1990,13(3):51-60. 被引量:3
  • 4Krier H, Burton R L, Pirman S R et al. Shock Initiation of Crystalline Boron in Oxygen and Fluorine Compounds. AIAA J., 1996, 12 (4) : 672 - 679
  • 5Foelsche R O, Spalding M J Krier H. High Pressure Ignition of Boron in Reduced Oxygen Atmospheres. ONR-AASERT Final Technical Report AAE 96-09, 1996
  • 6Foelsche R O, Burton R L, Krier H. Boron Particle Ignition and Combustion at 30 - 150atm. Combustion and Flame, 1999, 117: 32 - 58
  • 7Abdullah Ulas, Kenneth K. KUO and Carl Gotzmer. Ignition and Combustion of Boron Particles in Fluorine-Containing Environments. Combustion and Flame, 2001, 127 : 1935 - 1957
  • 8Mockenhaupt J D, Felix G J. Cold Flow Tests of Forced Deflection Nozzle for Integrated Stage Application. AIAA-81-1420
  • 9刘宝芬.固体推进剂的新发展..航空航天部科技情报研究所航天工艺材料简况.,1987(5)..
  • 10莫红军.固体推进剂发展新动向-满足火箭发动机高压工作的需求[J].火炸药动态,2004,(3):1-4.

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