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单词 hybrid rocket
释义

hybrid rocket

美 
英 
  • un.混合燃料火箭发动机
  • 网络混合式火箭;混合型火箭;混合火箭
un.
1.
混合燃料火箭发动机

例句

释义:
1.
If the hybrid rocket needs to be shut down in a hurry all you need do is turn off the pump delivering the oxidiser.
如果混合火箭发动机需要立即关掉,那么你需要做的全部事情就是关掉传送氧化剂的泵。
www.ecocn.org
2.
However, from what I gather, "hybrid" rocket engines use both solid and liquid or gas propellants.
然而我的理解是,“混合动力”火箭引擎同时使用固体燃料和液态或气态推进剂。
www.bing.com
3.
Another unconventional design element, the hybrid rocket engine that powers the suborbital vehicle, provides unique operational options.
另一个异于传统的设计要素,是提供次轨道载具动力的混合式火箭引擎,它能提供独特的操作选择。
dictsearch.appspot.com
4.
It was found that the aggregation method is suitable to treat solid fuel SQ in solid-liquid hybrid rocket.
研究发现固液混合火箭固体燃料SQ合适的处理方法为团聚法。
www.dictall.com
5.
They are fully reusable, burn cleanly, and release fewer particulates than solid fuel or hybrid rocket motors.
液态引擎与靠固体或混合燃料驱动的火箭马达相比,可以完全的回收利用,燃烧清洁,释放的污染物也少。
www.elanso.com
6.
There's actually another kind of hybrid: rocket engines.
事实上还有另外一种混合动力引擎:火箭引擎。
www.bing.com
7.
If we can go to space with improved hybrid rocket engines on half the fuel used now, that would be a giant step.
如果我能够坐在相当于只使用现今火箭所需一半燃料的改良型火箭上太空的话,那将会又是迈出了很大的一步。
www.bing.com
8.
Study on Improving Technological Properties of Solid Fuel SQ Formulation Used in Solid-Liquid Hybrid Rocket
固液混合火箭用固体燃料SQ型配方工艺性能改善研究
hxtjjygfzcl.nextage.cn
9.
Effects of combustion chamber structure on combustion and flow of hybrid rocket motor
燃烧室结构对固液火箭发动机燃烧与流动的影响研究
service.ilib.cn
10.
Numerical Simulation of Combustion Chamber and Nozzle Flow in Classical Hybrid Rocket Motors
固液混合火箭发动机燃烧室和喷管流动数值模拟
ilib.cn
1.
The Opportunity for Hybrid Rocket Motor in Commercial Space Applications
固液火箭发动机在空间发射上的应用前景
service.ilib.cn
2.
Fundamentals of Hybrid Rocket Combustion and Propulsion
固液混合火箭发动机燃烧原理
www.cnpbook.com
3.
Computation of combustion in hybrid rocket motor using a boundary layer theory
固液混合火箭发动机燃烧的边界层计算
service.ilib.cn
4.
The Performance Characteristic of Hybrid Rocket Engine
固液火箭发动机性能特征
www.ilib.cn
5.
Computation of fuel regression rate in classical hybrid rocket motors
固液混合火箭发动机固体燃料的燃速计算
www.ilib.cn
6.
Models of the Fuel Surface Regression Rate in Hybrid Rocket Motor
混合发动机燃面后退速率模型分析
www.ilib.cn
7.
Nozzle Flow Computation of Classical Hybrid Rocket Motors
固液混合火箭发动机喷管流动计算
service.ilib.cn
8.
Grain design for hybrid rocket engine with cluster type thrust chamber
带簇式推力室的固液火箭发动机装药设计
scholar.ilib.cn
9.
Optimization of grain design for hybrid rocket engine
固液火箭发动机装药设计优化
scholar.ilib.cn
10.
Regression rate calculation for the solid fuel surface of hybrid rocket motor based on fluid-solid coupling technique
基于流-固耦合的混合火箭发动机固体燃料表面退移速率计算
www.ilib.cn
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更新时间:2025/8/19 15:55:02