无烟推进剂

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

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 .

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 .

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

对微波衰减小的无烟推进剂的研究

Study of the Smokeless Propellent with Small Microwave Attenuation

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 .

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 .

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

CL-20基无烟NEPE推进剂的热行为

Thermal Behaviors of Smokeless NEPE Propellants with CL-20

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 .

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 .

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 .

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 .

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 .

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 .

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

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