两种相分离可以同时发生，但其对复合固体推进剂性能的影响不同。
The phase separation between the binder and plasticizer may seriously decrease the properties of the propellants.
作为吸气式发动机，其性能不仅取决于发动机本身结构和推进剂性能，与飞行状态也有密切的联系。
As the air-breathing engine, the performance of solid rocket ramjet is determined not only by structure of engine and the performance of propellant, but also by flight condition.
对金属化胶体推进剂的热力学、流变学、燃烧及燃烧效率等的分析研究表明，金属化胶体推进剂性能与金属粉末的添加量和金属半径有关；
The thermodynamics, rheology, combustion of metallized gelled propellants(MGPs) are analysed. It is showed that the performance of MGPs is related to the amount and grain size of metal power added.
分析了固液发动机推进剂的燃烧特性和发动机性能特性、与液体和固体火箭发动机的不同，以及研制的技术难度等。
The propellant feature of burning behavior and engine in hybrid engine, the differences to liquid and solid engine and the difficulties of technology in development were analyzed.
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.
在真空环境下，用氩为推进剂，得到了不同工况下发动机的性能参数。
In vacuum environment, the performances of the arcjet were tested under several conditions with argon as the propellent.
结果表明，键合剂改善RDX／HTPB推进剂力学性能的主要原因在于它们改善了RDX颗粒与HTPB粘结剂基体间的界面粘结效能。
The results show that primary action of bonding agent improving RDX/HTPB propellant mechanical property was bonding agent improving interface adhesive effect of RDX grain to HTPB binder.
尤其是硼酸酯化合物5527，能大幅度提高高温力学性能，是优异的丁羟推进剂新型偶联剂。
It is shown that compounds of borate especially borate 5527 is available to improve the mechanical performance of HTPB propellant at high temperature.
为了了解塞式喷管性能，采用固体推进剂对塞式喷管单元发动机进行了模拟实验。
To find out the performance characteristic of aerospike nozzle, the simulated tests were a aerospike engine unit using solid propellant.
经过改进的双基推进剂的机械性能使我们能够指望获得大燃烧面的药柱几何形状，从而得到大推力。
The mechanical properties of improved double-base propellants enabled one to envisage grain geometrics with large combustion areas and consequently high thrusts .
采用氩为推进剂，在真空室中进行了发动机的性能实验。
The performance experiment of arcjet was made in vacuum chamber and argon was chosen as the propellant.
测量与理论分析了复合推进剂的黏性与力学性能。
Composite propellant viscosity and mechanical properties were measured and analyzed theoretically.
介绍了用可水解粘合剂（PEGA）或热塑性弹性体（TPE）粘合剂制成的新型固体推进剂具有令人瞩目的少污染和可再生使用性能的实例。
At last the example of a new type propellant containing the hydrolytical binder (PEGA) or thermoplastic elastomer binder (TPE) which have little pollution and reusable properties is introduced.
在国内首次用粒铸工艺制备出了力学性能好、具有燃烧平台的浇铸改性双基弹性体(EMCDB)推进剂。
Elastomeric modified cast double base (EMCDB) propellant, which has good mechanical properties and plateau burning-effect, has been first successfully prepared by granule-casting in China.
本文用不同界面性质填料的推进剂，经单轴拉伸试验，研究偶联剂对不同填料提高推进剂力学性能的偶联效应。
By the uniaxial tensile test, the effect of coupling agents on mechanical properties of the composite propellant with fillers different in surface property is studied in this paper.
重点指出固化剂和氧化剂的微胶囊化包覆、复合粒子的制备等对提高推进剂的性能有重要作用。
The important effects of microencapsulated coating of the curing agent and oxidizer and preparation of composite particles to improve the properties of solid propellants are also showed.
分析了在硝胺改性双基推进剂中炭黑对其燃烧性能的影响。
The effect of carbon black on burning properties of modified nitramine double base propellant was detailed in this 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.
此外，还研究了TPUE对硝胺改性双基推进剂力学、工艺，能量和燃烧性能的影响。
In addition, effects of TPUE on the mechanical properties, technique properties, combustion and energy properties of nitramine modified double propellant are studied.
穆斯克还讨论了来自着陆第一级储备的推进剂 对性能的影响 的结果。
Musk also addressed the performance hitthat results from reserving propellant for landing the first stage.
贫氧推进剂燃速是固体火箭冲压发动机设计和性能分析的重要参数，也是对推进剂配方进行检验验收的主要指标。
The burning rate of the fuel-rich propellants is the parameter which is important for Ducted Rocket design and performance analysis and is main inspection criterions of propellant prescriptions.
结果表明：由于GAP粘合剂中侧链的影响，使推进剂力学性能水平较低，因而必须对其进行改性。
The results show that the mechanical property level of GAP based propellants is relatively low owing to the effects of side chain in GAP binder, thus, its molecular structure must be modified.
固体推进剂的性能将取决于分散混合后固体颗粒的尺寸。
The performance of solid propellants depends on the solid particle size after dispersive mixing.
介绍了新近研制成功的一种以螺旋压伸成型工艺制造的能量较高的低特征信号推进剂的主要性能，并重点讨论了研制的关键技术。
The major characteristics and key technology about a new propellant with high energy and low signature are described, it is successfully studied by the screw extrusion technology recently.
并对含纳米铝粉推进剂的燃烧性能、能量性能进行了测定。
The combustion performance and energy property of propellants containing nano-aluminum were also studied.
对聚氧化乙烯(peo)为粘合剂硝酸酯增塑的高能推进剂配方力学性能进行了研究。
The mechanical properties of propellants formulation, which contains PEO binder and is plasticized by nitrate ester were studied.
从推进剂的能量特性和燃烧性能的角度探索了硝胺(rdx、HMX)在低燃速丁羟推进剂应用的可能性。
An application investigation of the nitramine (RDX, HMX) to the low burning rate HTPB propellants was carried out in the view of energetic property and combustion performance.
本文研究了贮存温度对丁羟推进剂老化性能的影响。
In this paper, the effects of the storage temperature on the ageing characteristics of HTPB propellants have been studied.
实验结果表明，这种化合物具有改善推进剂燃烧性能和力学性能的双重作用。
The results have shown that the compound can improve both propellant mechanical properties and combustion characteristics.
实验结果表明，这种化合物具有改善推进剂燃烧性能和力学性能的双重作用。
The results have shown that the compound can improve both propellant mechanical properties and combustion characteristics.
应用推荐