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solid rocket

美英

un.固体火箭；固体燃料火箭
网络固体液料火箭；固体火箭马达；用固体燃料推进的火箭

solid rocket

英-汉网络释义

solid rocket

固体火箭

rocket啥意思谁知道告诉我谢谢_百度知道 ... sounding rocket 探空火箭 solid rocket 固体火箭 rocket test 火箭试验 ...

固体液料火箭

航海及海运专业词汇英语翻译(S) ... solid rivet 实心铆钉 solid rocket 固体液料火箭 solid rotor 整锻转子 ...

固体火箭马达

Bryan C兄~我上文从头到尾都没提到陆射万剑应使用 turbojet engine，我说的是改使用固体火箭马达(Solid rocket)不过的确如 …

用固体燃料推进的火箭

翻译词典... ... solid matte 固体锍, 固体冰铜 solid rocket 用固体燃料推进的火箭 solid thimble 缆索套环, 实心套环 ...

固态火箭系统

固态火箭系统(Solid rocket):就是用固体燃料的火箭马达…这东西UC时代都用在姿势控制喷嘴、小型飞弹多半也用这个。

例句：

The object was too light to be a brick , but it was the same density as a piece of foam from a solid rocket booster .

这一物体太轻了而不可能是一个砖，然而它和固体燃料助推器上的泡沫的密度是相同的。

This article introduces a designing means of mold of the fibre winding solid rocket motor combustion chamber shell .

介绍一种固体火箭发动机燃烧室壳体纤维缠绕芯模的设计。

The test and measurement of the solid rocket motor (SRM) are important parts of the technology of solid-rocket propulsion .

固体火箭发动机地面试验与测试技术是固体火箭推进技术的重要组成部分。

But in launch position , the orbiter is perched on the side of its 15 -story external fuel tank and flanked by two solid rocket boosters .

但在发射点，轨道器一面是 15 层楼高的外挂燃料箱，两侧是两个固体火箭助推器。

In this paper the RBF neural network is applied to predict the cost of the solid rocket motor .

尝试将其应用于固体火箭发动机成本预测中。

China already has such segmented solid rocket motor and ramjet capabilities today, but scramjets are a much greater challenge .

中国已经拥有这种分离式火箭助推器和冲压发动机技术，但超音速燃烧冲压发动机是一个更大的挑战。

Did one of the solid rocket boosters somehow burn through its casing ?

是否是其中一个助推火箭的外壳因某种原因被烧穿？

The influences of mass warp, aerodynamic resistance warp and solid rocket-ramjet engine thrust warp on the flight velocity are analyzed .

研究了靶弹质量偏差、气动阻力偏差和冲压发动机推力偏差对飞行速度的影响。

It was considered that the establishment of radiographic IQI standard for solid rocket motor chamber was necessary .

认识到建立固体火箭发动机燃烧室 X 射线探伤像质计标准势在必行。

NASA 's Space Shuttle Program conducted the final test firing of a reusable solid rocket motor Feb. 25 in Promontory , Utah.

2月25日，美国航天局航天飞机组在犹他州海角对可回收的液态火箭引擎进行了最后的测试。

On the base, the paper analyses the structural integrity of solidification and launching in low temperature of Solid Rocket Motor .

主要研究内容如下：介绍了固体发动机结构完整性分析的概念及研究进展。

Along with the applications of the high-tech on solid rocket motors , the systematic complexity improves day by day .

随着高新技术在固体火箭发动机系统的不断运用，使其复杂性也日益提高。

Introduced the Method of electronic optical data high speed acquisition of ultraviolet radiation of solid rocket plume .

详述了固体火箭羽烟紫外辐射的光电高速采集方法，并实时对导弹逼近告警。

Supposedly , it was developed by NASA as a solid rocket fuel .

据说，这种东西最早是由 NASA 作为固体火箭燃料而研发的。

The mean flow fields in fore combustion chamber of solid rocket motors with grain regression were studied .

对具有燃面减退的固体火箭发动机燃烧室头部的内流场进行了研究。

The paper introduces a new method of measuring combustion time with CAT technique for solid rocket engine .

介绍一种应用 CAT 技术确定固体火箭发动机燃烧时间的新方法。

The inflation system is not unlike a solid rocket booster.

充气系统不像一个固体的火箭加速器。

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