无烟推进剂
- 网络smokeless propellant
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含能添加剂DNP对无烟推进剂性能的影响
The effect of energetic addition DNP on properties of smokeless propellant
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由此可见,TN确是一种高能氧化剂。本文还对TN、HTPB系列的无烟推进剂做了初步探讨。
The paper also did an initial research on the energetic characteristics of composite solid smokeless propellant consisted of TN and HTPB .
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以HCO取代HMX作为无烟推进剂的高能添加剂,其理论比冲都高于HMX无烟推进剂。
Smokeless propellants with HCO all show to give higher specific impulse ( theoretical ) than those with HMX .
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三种无烟推进剂压力耦合响应函数的实验研究
Experimental studies on the pressure coupling responses of three smokeless solid propellants
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对微波衰减小的无烟推进剂的研究
Study of the Smokeless Propellent with Small Microwave Attenuation
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硝酸铵(AN)是低特征信号推进剂和无烟推进剂的首选氧化剂,但存在点火、燃烧困难等问题。
Ammonium nitrate ( AN ), used as oxidizer of low signature and smokeless propellants , is a promising candidate . However there are some problems for AN-based propellant in ignition and combustion .
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用压力可控T形燃烧器测量了三种无烟推进剂压力耦合响应函数,总结到一些实验规律,提出燃烧催化剂对抑制不稳定燃烧可能起到的重要作用。
Using pressure-controlled T-burner the anthors have determined the pressure coupling responses of three smokeless solid propellants . From the experiment results we have believed that the combustion catalyst may play an important role in eliminating the combustion instability in a solid rocket motor .
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铅盐对无烟NEPE推进剂燃烧性能的影响
Effects of Types of Lead Compounds on the Combustion Characteristics of Smokeless NEPE Propellants
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CL-20基无烟NEPE推进剂的热行为
Thermal Behaviors of Smokeless NEPE Propellants with CL-20
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利用热重(TG-DTG)和高压差示扫描量热(PDSC)研究了含与不含CL-20的无烟NEPE推进剂的热行为。
The thermal behaviors of the smokeless NEPE propellants with and without CL-20 are studied by TG-DTG and PDSC .
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针对浇铸中能无烟RDX-CMDB推进剂配方,进行了催化剂对燃烧性能影响的研究。
The influence of combustion catalysts on the combustion properties of casting RDX CMDB propellants with middle energy is studied in present paper .
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研究了不同工艺对含ACP无烟改性双基推进剂燃烧性能的影响。
The effect of different technology including casting and extrution on the combustion performance of smokeless modified double-base propellant with ACP was studied .
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含ACP的无烟改性双基推进剂能量特性理论计算表明,ACP对推进剂的能量影响较小。
The theoretical calculation results of energy characteristics for smokeless modified double-base propellant with ACP show that ACP can decrease the energy of the propellant .
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分析了ACP提高无烟改性双基推进剂燃速的作用机理,认为ACP可增加燃烧表面积和热量向燃烧表面积的反馈,使推进剂的燃速大增。
It is considered that the combustion surface and the heat feedback of the propellant are increased by addition of ACP , leading that the increasing of burning rate of the propellant .
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实验结果表明,ACP对压伸工艺制备的推进剂燃速没有显著提高,但能大幅度地提高浇铸无烟改性双基推进剂的燃速。
The results show that ACP can increase the burning rate of the casting propellant , while ACP can not increase the burning rate of the extrusion propellant , obviously . The mechanism of increasing the burning rate of the propellant by ACP was experimentally analyzed .
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硝胺无烟改性双基推进剂燃烧性能调节及控制规律的初探
A research on combustion properties adjustment and control for smokeless Nitramine Propellant
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高压平台浇铸无烟改性双基推进剂综合性能研究
The Studies of Synthetical Properties on Casting Smokeless CMDB Propellants with High Pressure Plateau Combustion