该方法可以快速地进行多级火箭的飞行方案设计。
This approach is efficient for flight program design of multi-stage rockets.
经过金星还有经过火星的其他飞行方案也计划出了。
提出了一种进行单级和多级火箭飞行方案设计的一般方法。
A generalized approach to flight program design for single and multi-stage rockets are presented.
基于模拟的飞行方案，项目人员已经完成了一次所有推进器的按序点火测试。
Project handlers have already carried out a firing test on all the thrusters, firing them in series based on a simulated flight scenario.
讨论了空中发射运载火箭的基本特点、飞行方案、发射轨道设计和优化分析方法。
The essential characteristics, flight sequence, trajectory design and optimal analysis for air launch vehicle are discussed.
美国和欧洲的安全专家正在着手建立覆盖面广阔的飞行数据库，希望以此获得安全系数更高的飞行方案。
Safety experts in the U. S. and Europe are establishing vast databases of flights to determine how flying can be made safer.
系统为用户提供大量的、可视化的仿真结果，从而协助他们完成飞行方案的设计、验证、论证、筛选和确定。
The system can give user plentiful and visually result of simulation; consequently help them accomplish the design, validation, argumentation, filter and decision of flight scheme.
而正在进行的这一系列测试飞行，其实是为了给用来实现环球飞行的第二架飞机……HB-SIB确定最终设计方案。
The series of test flights which it is undertaking are being used to set the final design for a second aircraft, HB-SIB, which will be used to make the global flight.
我们将优惠飞行预订解决方案的示例划分为业务逻辑(在WebSphereProcessServer中开发和部署)和连接性逻辑(在WebSphere ESB中开发和部署)。
The example of an award flight reservation solution was split into business logic (developed and deployed in WebSphere Process Server) and connectivity logic (developed and deployed in WebSphere ESB).
报告的完整版本将提供对摘要报告里的五个方案的详细比较——其中包括一项以在最终完成火星轨道飞行为目标的计划。
The full version will provide a detailed comparison of the five options presented in the summary report – including one plan that would culminate in a trip to Mars orbit.
他们提出了一套方案以替代星座计划，即根据载人飞行目的地的不同而使用不同的火箭。
They presented a series of alternatives to Constellation that would send humans to different destinations and use different rockets.
EPLRS网络为士兵评估从无人飞行器到其他传感器架设网络的方案提供了端到端的联接。
The EPLRS network provided end-to-end connectivity for soldiers to evaluate networked solutions from unmanned aerial vehicles and other sensors.
研究人员还需要一个成熟的方案来确保飞行器保持正直。
Researchers also need a sophisticated solution to make sure the robot remains upright.
在这个方案中，一个载物飞行器(比如说搭载着卫星)将(首先)搭载超燃冲压发动机进入相当高度，理论上能够达到近似轨道速度。
In such a scheme, a payload vehicle (holding, say, a satellite) would piggyback to high altitude aboard the scramjet, which in theory could reach near-orbital speeds.
Serghides博士在模拟器上进行了设计方案模式飞行，结果良好。
Dr Serghides has flown his design in a simulator and says it handles well.
普惠公司现在要做的就是将试验飞行中获取的数据进行整理分析，最终敲定发动机的设计方案。 PW1000G发动机计划在2013年投入使用。
P&W will now use the data gathered from its test flights to finalise the engine’s design.
这事个很好的方案，他们不可能远离你直到飞行的结尾。
The good thing of this scenario, is that they can not run away from you until the end of the flight.
使用飞行模式可以关闭所有无线连接，在网络不好的地方，这是最便捷、最省事的解决方案。
Airplane Mode, an option that will turn off all wireless features, is a quick and easy solution in areas with poor reception.
RBCC发动机性能分析模型在高超声速飞行器方案选择、总体设计以及RBCC发动机设计与性能分析等方面具有极其重要的作用。
RBCC engine performance analysis model plays an important part in scheme selection and model design for Hypersonic Flight Vehicle, RBCC engine design and performance analysis.
该方案非常适用于现代武器低空飞行时的导航。
It can be applied in the navigation system of the modern weapon which is flighting at low altitude.
因此，有必要对亚音速飞行器的导航方案进行改进。
Therefore, it is necessary to improve the current navigation means of the subsonic vehicle.
除了一些常规的装甲环节和配色方案上的不同，AT-AT驾驶员的制服与钛战机飞行员制服颇为相似。
The uniform of the AT-AT pilot is mostly similar to that of a TIE fighter pilot, except with some custom armor segments and a different color scheme.
提出了弹上无线电高度表因外因导致高度指示异常时，使导弹具有一定的自适应能力，避免导弹飞行试验失败的改进方案。
The improving measures are proposed to make the missile possess a certain adaptive ability avoiding the failure of missile flight test when the missile borne radio altimeter is out of order.
通过对雷达昆虫学研究和其他方法得到的研究成果的综合分析，提出一套昆虫迁飞行为参数化方案。
A parameterizing scheme for insect migratory behaviour was presented based on the comprehensive analysis of the radar entomological researches and other migration studies.
在常用坐标系下，推导了空间运动的数学模型，设计了方案飞行弹道。
Under the usual coordinates, the paper conclude mathematical model in space motion and design project ballistic trajectory.
介绍了主发动机加助推器和简易控制方法实现固体火箭等高飞行的设计方案。
The tentative design of constant altitude flight solid rocket composed of the sustainer, the booster and its simple control method is presented.
介绍了主发动机加助推器和简易控制方法实现固体火箭等高飞行的设计方案。
The tentative design of constant altitude flight solid rocket composed of the sustainer the booster and its simple control method is presented.
介绍了主发动机加助推器和简易控制方法实现固体火箭等高飞行的设计方案。
The tentative design of constant altitude flight solid rocket composed of the sustainer the booster and its simple control method is presented.
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