双基推进剂

改性双基推进剂主要组分的高压热分解特性

Thermal Decomposition Characteristics of Several Main Ingredients Used in CMDB Propellants

直链叠氮硝胺对双基推进剂燃烧性能的影响

Influence of some straight chain azido - nitramine on combustion properties of CMDB propellant

TG分析法研究双基推进剂的热分解反应动力学

Reaction Kinetics Research on Thermal Decomposition of DB Propellant with TG Analytical Method

含RDX改性双基推进剂基础配方及其燃速探索

Studies on Foundational Formulation of Composite Modified Double Base Propellant Containing RDX and its Burning Rate

用PDSC和TG-DTG研究了RDX-CMDB改性双基推进剂在一种含能复合燃速催化剂作用下的热分解。

The thermal decompositions of RDX-CMDB modified double base propellants with a composite burning catalyst were investigated by using of PDSC and TG-DTG .

含CL-20的改性双基推进剂燃速数值模拟

Numerical Simulation for Burning Rate of Composite Modified Double Base Propellant Containing CL-20

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 .

SJ-1双基推进剂老化性能的动态力学表征

Dynamic mechanical characterization of aging properties for SJ-1 double base propellant

初步研究表明，四唑类的金属盐类可以作为复合改性双基推进剂（CMDB）的含能燃烧催化剂。

The experimental results suggest that the salts are good energetic catalysts of composite modified double-base ( CMDB ) 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 .

结果表明，FOX-7与改性双基推进剂的主要组分具有良好的相容性；

The results show that the binary systems of FOX-7 with the main components of CMDB propellant have good compatibility .

DNTF代替具有平台燃烧特性的改性双基推进剂中的RDX后，推进剂仍可获得较低的压强指数。

When the ingredient RDX of the composite modified double base propellant with plateau effect was replaced with DNTF , the propellant still possesses lower pressure exponent .

FOX-12改性双基推进剂只有一个分解峰，表明FOX-12和双基黏结剂（NC、NG等组分）一起分解。

There is only one exothermic peak of FOX-12-CMDB propellant , showing that FOX-12 and double base binder ( NC and NG , i.e. ) are decomposed at the same time .

用高压差示扫描量热法（PDSC）研究了五种含RDX改性双基推进剂RDX-CMDB在不同压力下的热分解特征量及其与燃速的关系。

The thermal analysis characteristics and their relationship with burning rate at various pressures for five RDX-CMDB propellants were investigated by high pressure Differential Scanning Calorimetry ( DSC ) .

硝酸酯增塑聚醚推进剂又简称NEPE推进剂，是一种集改性双基推进剂和复合推进剂的优点于一身的固体推进剂，由于具有能量高和低温力学性能好等优点被广泛的使用。

Nitric acid ester plasticized polyether ( NEPE ) propellant has a good advantage of high energy and low temperature mechanical properties , which has the characteristic of modified double-base propellant and composite propellant .

采用相对光强度法测定了双基推进剂、复合推进剂及NEPE（氧化剂为HNIW或HMX）推进剂的燃烧火焰温度分布。

Temperature distribution of combustion flame of double base propellant , composite propellant and NEPE propellant ( taking HNIW or HMX as oxidizer ) were measured by using relative light intensity method .

用快燃物ACP提高改性双基推进剂、AP/HTPB复合推进剂和N-15D推进剂的燃速，取得了非常显著的效果。

Extraordinary and outstanding effect of improving the burning rate of modified double-base propellant , AP based composite propellant and N-15D propellant was achieved with fast-burning energetic material ACP .

采用动态热机械分析法测定了SJ-1双基推进剂的动态力学性能，表征了其在65℃下的老化性能。

The dynamic mechanical properties of SJ-1 double base propellant were measured by means of dynamic mechanical analysis methods , and aging properties at 65 ℃ were characterized .

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 .

增塑剂对双基推进剂动态力学性能的影响

Influence of plasticizers on dynamic mechanical properties of double base propellants

提高螺压双基推进剂能量的探讨

Discussion on enhancing the energy of screw extruded duble base propellant

双基推进剂硝胺脱湿及其键合剂分子设计

Molecular Design of the Bonding Agent for Double Base Propellant

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

少烟复合改性双基推进剂燃烧性能研究

A Study of Combustion Characteristics of Reduced Smoke Composite Modified Double-Base Propellant

三种挤压成型的改性双基推进剂的安全特性

Safety Characteristics of Three Extruded Composite Modified Double Base Propellants

改性双基推进剂冲击波响应过程的研究

Response of High Energy Modified Double - Based Propellant to Shock Loading

改性双基推进剂老化燃烧性能实验研究

Investigation on Combustion Property of accelerated aging CMDB solid propellant

双基推进剂燃烧过程中二氧化氮对推进剂的作用

The effects of NO2 on the Combustion Process of Double Base Propellants

双基推进剂火箭排气羽流的微波衰减

Microwave Attenuation of the Exhaust Plume for Double-Base Propellant Rockets