rocket propellant

1. The Method of Hazard Assessment Applied to Liquid Rocket Propellant Operation
   危险评价方法及在液体火箭推进剂作业中的应用
2. The pattern of liquid rocket propellant seep and steam diffusion is discussed in this paper, and the model of quantitative analysis is also established.
   讨论了航天发射场液体推进剂泄漏及蒸汽逸散的模式，并建立了定量分析模型。
3. Design of Rocket Propellant Regeneration Equipment Based on Distributed Control System
   基于集散控制系统的火箭推进剂再生装置的设计
4. A chemical agent added to a material, such as rocket propellant, to make it opaque.
   在物质中添加一种化学添加剂，如加在火箭助推器中，使之不反光。
5. Virtual Machine Tool Technology for Solid Rocket Propellant
   用于固体火箭推进剂的多功能集成虚拟机床技术
6. With electric energy as the energy source, electromagnetic launcher is much cheaper to use than rocket propellant using gunpowder.
   电磁推进器使用电能作能源，远比火箭推进剂和火炮火药的成本低；
7. Objective To investigate effect of combine using Naloxone and Promethazine on mice intoxicated by rocket propellant ( UDMH).
   目的本文探讨纳洛酮联用盐酸异丙嗪对火箭推进剂偏二甲基肼（UDMH）中毒鼠的救治效果，以探讨简便易行的对UDMH中毒防治的新途径。
8. Application of closed burner for measuring burning rate of solid rocket propellant
   密闭燃烧器在固体火箭推进剂燃速测定中的应用研究
9. The atomization mechanism of hypergolic rocket propellant and decomposition combustion at high pressure and turbulence burning of premixed reactant flow field are considered.
   数值仿真模型中考虑了自燃推进剂雾化机理、高压分解燃烧和预混反应流湍流燃烧等。
10. A real-time temperature measurement device for rocket propellant is designed according to similarity criterion.
    在相似原理基础上设计了火箭推进剂实时温度测量装置。
11. Numerical Research on Transient Temperature Field Characteristics of 130 Rocket Propellant
    130火箭推进剂非稳态温度场特性数值研究
12. In the present paper, the structure features, synthesis method and thermolysis performance of CL-20 are reviewed. And the energetic performance of CL-20 used as solid rocket propellant oxidizer is calculated as well.
    综述了CL－20结构特征、合成方法及热分解性能，并对其作为固体推进剂氧化剂的能量特性进行了计算分析。
13. This paper did some research on numerical simulation about the structure of solid rocket propellant, based on the mechanical problem during the designing process and stockpile process of solid rocket propellant.
    本论文以固体火箭发动机在设计和贮存使用过程中所常见的力学问题为研究背景，对固体推进剂材料的特性结构的数值仿真作了多侧面的研究。
14. This research aimed at the fatalness for using liquid rocket propellant in our country spaceflight launch site, applied the principle of safe system engineering to analysis the dangerous factors.
    本研究针对我国航天发射场液体火箭推进剂作业中存在的危险性，利用安全系统工程原理，对推进剂作业的危险因素进行了系统分析。
15. Theoretical and experimental studies for liquid rocket propellant explosion
    液体推进剂爆炸理论与实验研究
16. On Burning Rate Measurement System of Solid Rocket Propellant in a Closed Burner
    密闭燃烧器法固体推进剂燃速测试系统
17. Analysis of liquid rocket propellant evaporation characteristic in natural environment
    液体火箭推进剂在自然环境中蒸发特性
18. Firstly, the paper introduced development of large vehicle rocket propellant and presented current directions of monitoring tech for propellant and tendency of digital signal processing system meantime technical requests and system index were given in this paper.
    本文首先从课题的研究背景出发，综述了大型运载火箭推进剂的发展过程，介绍了加注液位检测技术的研究现状和数字信号处理系统的发展动态，给出了该系统的性能指标和技术要求。
19. The application of melamine phosphate as filler in the insulating layer on a rocket propellant charge, mechanism of its action, its protection mode against fire, its compatibility with the insulating layer matrix and its other advantages were introduced.
    介绍三聚氰胺磷酸盐作为填料在推进剂绝热层中的应用及其作用机理、对火的防护模式、与绝热层基体材料的匹配性和其他优异性能。
20. The calculation of energy dissipation and heat of solid rocket propellant grains subjected to vibration
    固体火箭推进剂在振动过程中的能量耗损和热量计算
21. The Study and Development of Skin Protective Equipment for Liquid Rocket Propellant
    火箭推进剂皮肤防护装备研究现状及发展趋势
22. Solid rocket propellant is a kind of high-energy material. Therefore, the propellant is easy to combustion and detonation.
    固体推进剂是一种高含能材料，具有燃烧和爆炸的危险性。
23. The Quantitative Safety Analysis of Conventional Liquid Rocket Propellant Operation
    常规液体推进剂作业安全性研究
24. Off-axis holographic investigation of particle fields of solid rocket propellant combustion
    固体火箭推进剂燃烧粒子场的离轴全息研究
25. Development in the Preparation of Nano-scale Combustion Catalysts Used in Solid Rocket Propellant
    固体推进剂用纳米燃烧催化剂制备研究新进展
26. By studying and summing up the failure physical models in common use, this paper advanced a cumulative damage-reaction theory life model to the storage and usage of solid rocket propellant, and, by calculating examples, demonstrated this model clearly.
    通过对常用失效物理模型的分析和总结，提出了固体火箭推进剂贮存使用寿命的累积损伤-反应论模型，并通过算例阐释了这一模型。
27. According to the requirements from the projects, electric probes are applied for the electron density, temperature and collisional frequency in the ground experiment facility of flight circumstances, the components of solid rocket propellant testing device and sintered Shockwave tube.
    根据项目要求，本文分别在飞行环境地面实验装置、固体助推剂成分实验装置和粉末激波管上使用静电探针完成了电子密度、电子温度和碰撞频率等参数的测定。
28. In industrial piping systems, such as the heat exchanging and circular system of the nuclear power station, and the rocket propellant piping, etc* The water hammer take placed frequently for the opening and closing of the valve.
    在工业管道中，如：核电厂的热力交换和循环系统，火箭推进剂输送系统等等，由于阀门的开启和关闭经常会产生水锤现象。

noun

1. an explosive charge that propels a rocket

   Synonym:    rocket fuelrocket propellent