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- rocket propellant tank 火箭推进剂贮箱
- This thesis conducts a PLC-controlled automatic washing system for the rocket propellant stirrer tank. 基于PLC的火箭推进剂搅拌罐清洗系统。
- A rocket propellant consisting of a single substance or mixture that contains both fuel and oxidizer. 单元推进剂一种含有单一物质或燃料和氧化剂混合物的火箭推进剂
- Propellant tank and high pressure vessel are important component of satellite prolusion system. 推进剂贮箱、高压气瓶(简称贮箱、气瓶)是卫星推进分系统的重要核心部件。
- A colorless, oily liquid, CH3NO2, used in making dyes and resins, in organic synthesis, and as a rocket propellant. 硝基甲烷一种无色的、油质液体CH3NO2,用来制造染料和合成树脂,用于有机合成,以及作为火箭助推剂
- The inner part of the propellant tank is one ultra thin TB8 spherical part which is made of two hemispherical parts by welding technique. 推进系统贮箱内层为超薄TB8钛合金球形件,由两个半球件焊接而成。
- A two - component rocket propellant,such as liquid hydrogen and liquid oxygen,fed separately to the combustion chamber as fuel and oxidizer. 二元燃料一种二元火箭燃料,如液氢和液氧,作为燃料和氧化剂分别加入燃烧仓
- A two-component rocket propellant, such as liquid hydrogen and liquid oxygen, fed separately to the combustion chamber as fuel and oxidizer. 二元燃料一种二元火箭燃料,如液氢和液氧,作为燃料和氧化剂分别加入燃烧仓
- Inside the bucket, xenon gas from the propellant tank flows into an ionization chamber where an electromagnetic field tears electrons off the xenon gas atoms to create a plasma. 在这个光电桶中,氙气由推进剂槽流入离子化室,离子化室中的电磁场使气态氙原子的电子脱离,形成电浆。
- An experimental test apparatus and procedure for measuring erosive burning rates of solid rocket propellant is described in the present paper. 该文描述了一种固体火箭推进剂侵蚀燃烧的测试方法。
- 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。
- Chemical rockets create their exhaust by the combustion of rocket propellant. 化学火箭由火箭燃烧推进燃料所产生气体推进。
- The very model can be used as a theoretic gist in forecasting the useful life of solid rocket propellant in varying environment,or as a referable model for the calculation of the residual life of SRM. 文中所述的模型可作为变化环境下固体火箭推进剂贮存使用寿命预估的重要理论依据,也可作为固体火箭发动机剩余寿命计算的参考模型。
- The chief exception was lengthened second-stage propellant tanks to increase the payload by 300 kilograms. 一个主要的例外就在于将第二阶段的推进箱加长,以便增加300千克的载重量。
- Then, by choosing the control weighted matrix R reasonably, the constrained optimization problem as formation keeping with electric rocket propellant can be transformed into the unconstrained optimization to be solved. 然后通过合理的选择控制加权矩阵R,用无约束的线性二次型优化方法解决了电推力火箭有控制约束的优化问题。
- Drying way selection of propellant tank 推进剂贮罐干燥方式的选择
- DESIGN OF WELL-WASHER WITH SOLID ROCKET PROPELLANT 固体火箭推进剂洗井器设计
- Our pilotless rocket enters the track of the earth. 我们把一个无人驾驶的火箭送入了地球的轨道里。
- Study of monitoring system for propellant tank status 推进剂贮罐状态监测系统的研究