hypergolic的例句大全

Study shows this new bipropellant have good hypergolic and fire performance.

研究表明，过氧化氢/醇类这种新型双组元推进剂具有良好的自燃和点火特性。

Variable Gain Solenoid Valve Control System Used for Hypergolic Bipropellant Variable Thrust Rocket Engine

用于双组元自燃推进剂变推力火箭发动机的可变增益电磁阀控制系统

A combustion model for the high-pressure liquid hypergolic bipropellant rocket engine

高压自燃双组元液体火箭发动机燃烧模型

The High-Pressure Equilibrium Vaporization Model of a Hypergolic Propellant Species Droplet

自燃推进剂组元液滴的高压平衡蒸发计算模型

Hypergolic Research of Hydrogen Peroxide with Alcohols Green Bipropellant

过氧化氢/醇类绿色双组元推进剂自燃技术研究

Green Hypergolic Bipropellant Using Hydrogen Peroxide as an Oxidant

绿色过氧化氢双组元自燃推进剂

Hydrogen peroxide/ azido-amine combination is hypergolic bipropellant with high density specific impulse.

过氧化氢/叠氮胺类不但密度比冲高，而且可实现自燃；

Several bipropellant chambers were designed and produced, and the hydrogen peroxide/ kerosene hypergolic ignition characteristics were studied with 500 firing tests.

设计并生产了几种双组元推力室，对过氧化氢/煤油自燃点火技术进行了研究，累计进行了500余次点火试验；

A mathematical model describing combustion in a high pressure liquid hypergolic bipropellant ( UDMH/ H2O4) rocket engine combustor has been developed.

本文提出了一个高压液体双组元自燃推进剂火箭发动机燃烧室计算模型。

To make concrete with aggregate of hypergolic coal jamb will usually bring on a higher sulphur content and result rest of the reinforcing bar, thus a popular use of the coal jamb becomes difficult.

用自燃煤矸石集料制作混凝土，常常遇到硫含量偏高，导致钢筋锈蚀，从而影响煤矸石混凝土的推广应用。

Under the same temperature and the chamber pressure, hypergolic ability of transverse injectors is better than that of the gas/ liquid coaxial injectors. Hypergolic ability tends to improve with higher nozzle contraction ratio.

在相同温度和室压下，横向喷注器的自燃能力优于气液同轴喷注器，喷管收缩比越大，越利于自燃。

The effect of initial propellant temperature on rocket engine combustion stability for hypergolic propellant ( MMH/ NTO) is studied. A physics model for initial propellant temperature effecting evaporation rate has been developed in this paper.

对自燃推进剂（MMH/NTO）初始温度对火箭发动机燃烧稳定性的影响进行了研究，从推进剂初始温度对蒸发速率的影响规律出发，发展了初始温度大小影响蒸发速率的物理模型。

The lighter version used liquid hydrogen, the heavier used hypergolic propellants.

较轻的推进器采用液态氢, 较重的采用自燃推进剂.

Hypergolic ignition systems bear many resemblances to hybrid rockets.

自然式点火系统在很多方面与混合型火箭相似.

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。