复合推进剂

湿度对HTPB复合推进剂力学性能的影响

Effect of Humidity on Mechanical Property of HTPB Composite Propellant

国产HTPB复合推进剂裂纹扩展特性的实验研究

Experimental research on crack growth behavior in HTPB Composite Propellant

AP/HTPB复合推进剂用纳米Co粉的制备

Preparation of Co Nanometer Powder Used for AP / HTPB Propellant

实验研究了纳米级Al粉（包覆）和微米级Al粉在复合推进剂中对燃速及压强指数的影响。

The effects of coated nano-sized Al powder and micron-sized Al powder in propellants on the burning rate and pressure exponent have been investigated .

某些化合物对HTPB复合推进剂燃速压力指数的影响

Effect of Some Compounds on HTPB Composite Propellant Burning Rate Pressure Exponent

通过常温湿度试验，研究了HTPB复合推进剂力学性能随试验时间的变化规律。

The change rule of mechanical property of HTPB composite propellant with test time was studied by humidity test .

介绍了国外对GAP／AN复合推进剂燃烧性能研究的新进展，探讨了少量添加剂对GAP／AN推进剂燃速特征的影响，评价了GAP／AN推进剂的钝感性能。

This paper describes the recent development in research of combustion characteristics of GAP / AN composite propellants . The effect of additives on the combustion performance is discussed . The sensitivity performance is evaluated .

国外含ADN或HNF的高能复合推进剂

High Energy Composite Propellant Containing ADN and HNF at Abroad

本文研究了RDX/AP配比对其HTPB复合推进剂爆温（Tv）、燃烧产物中HCl含量、燃速和燃速压力指数的影响。

In this paper , the effects of RDX / AP proportion on deflagration temperature ( Tv ), Hcl content in combustion products , burning rate and burning rate pressure exponent have been studied .

本文主要针对某AP/HTPB底排复合推进剂的点火燃烧性能进行了研究，并计算分析了A1化AP/HTPB复合推进剂的燃烧特点。

In this paper , the characteristic of ignition and combustion on a AP / HTPB composite propellant is studied , in addition , analyzing the characteristic of combustion on the propellant containing aluminum .

该模型可用于包括易熔粘合剂在内的AP复合推进剂。具有能说明平台、mesa和正常的燃烧行为，分析初温、AP颗粒尺寸对燃烧特性影响的能力。

The model is developed for AP-based composite solid propellants can be used to explain plateau , mesa and normal burning behavior and to analyse the effect of initial temprature and AP particle size on burning behavior .

BAMO-THF复合推进剂能量特性计算与分析

Calculation and Analysis on Energy Characteristics of Composite BAMO-THF Propellants

应用热分析方法研究了CuO、Cr2O3、Co2O3及其碳酸盐的煅烧产物对AP／HTPB复合推进剂凝聚相反应热效应的影响。

The influence of CuO , Cr_2O_3 , Co_2O_3 and calcined products of these carbonates on AP / HTPB composite propellant condensed phase thermal effect are investigated in this papaer .

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 .

考虑了AP／RDX／HTPB推进剂中两种氧化剂的含量、配比和粒度对推进剂燃面结构及燃速的影响，建立了一个高氯酸铵／硝胺复合推进剂的双区稳态燃烧模型。

A " Two Zone " steady combustion model of AP / nitramine composite propellant was developed , considering the effect of the contents and particle sizes of the two oxidizers on the surface structure and burning rate of the propellants .

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 .

根据异质推进剂的特点，提出了含氧流动热气体点燃PBAA复合推进剂的气相点火模型。

This paper describes the gas-phase ignition model of composite solid propellants ignited by oxygen-contained flow hot gases according to the characteristics of heterogeneous propellants .

调整复合推进剂配方改善喷焰微波衰减特性

Tailoring Formula to Improve Microwave Attenuation Characteristics of Composite Propellant Plume

复合推进剂微裂纹损伤本构模型研究

Study on micro-cracking damage constitutive model of HTPB composite solid propellent

高氯酸铵/硝胺系复合推进剂燃烧特性研究

Characteristic study of combustion for ammonium perchlorate / nitramine composite propellants

HTPB/AP复合推进剂冲击波点火实验研究

Research of HTPB / AP Composite Propellant Shock Wave Ignition

关于硝胺复合推进剂燃速特性和燃烧模型的述评

Review of burning rate characteristics and combustion mechanisms for nitramine composite propellants

硝胺/丁羟复合推进剂高效偶联剂

The high efficient bonding agents for hmx / htpb solid composite propellant

含铝复合推进剂燃速计算研究

A calculation research on burning rate of aluminized composite propellant

复合推进剂中硝酸铵的改性研究

Study on modification of ammonium nitrate in the composite propellant

高氯酸铵/硝胺丁羟复合推进剂热感度及机械感度研究

Research on thermal and mechanical sensitivity of AP / nitramine HTPB propellant

HTPB/AP/Al复合推进剂燃速降速剂研究

Study on Burning Rate Inhibitors of HTPB / AP / Al Propellants

加速度对含铝复合推进剂燃烧的影响

The effect of acceleration on the combustion of aluminized composite solid propellants

丁羟复合推进剂粘弹力学特性主曲线

Master curves for viscoelastic properties of HTPB Composite Propellants