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Uusing ISRO's Geosynchronous Satellite Launch Vehicle MkIII rocket to launch the capsule, the organisation's chairman G Madhavan Nair says preliminary study work has been under way.

ISRO官员称,除了将满足印度航天局2015年载人太空飞行任务的需要,该发射台还将设计用来发射被提议的可复用运载火箭——印度梦想中的航天飞机。

In science and technology to achieve the first of the four, it is necessary to develop and launch China's first extraterrestrial objects and the landing detector detectors to inspect for the first time the use of the "Long March Route B" on the transfer of launch vehicle and spacecraft orbit for the first time The establishment and use of deep-space monitoring and control network for monitoring and control communications, for the first time to achieve a soft landing on the moon, the face on tour, the Spring River, and so the survival of a major breakthrough, carried out on tables topography and geological structure, mineral composition and chemical composition of the internal structure of the moon, the earth-moon Table on the environment and space exploration, and other activities supporting the basic completion of the lunar exploration engineering system.

在科学技术方面,实现四个第一,要研制并发射中国第一个地外天体着陆探测器和巡视探测器,第一次利用"长征三号乙"运载火箭发射地月转移轨道航天器,第一次建立和使用深空测控网进行测控通信,第一次实现月球软着陆、月面巡视、月夜生存等重大突破,开展月表地形地貌与地质构造、矿物组成和化学成分、月球内部结构、地月空间与月表环境等探测活动,建成基本配套的月球探测工程系统。

The national defence basic project as background and the dynamic model of cotrolled transfer matrix for multiple launch rocket was created in order to reduce the initial disturbance of rocket projectile. The causes that affect the angle change of orientation locator were analyzed by the engineering system dynamic theory base on multibody system transfer matrix method. The simulation of dispersion for multiple launch rocket was implementation, and the affect law between the angle of elevation and side deflection and the control parameters was acquired. The control module was installed on the orientation locator of multiple rocket launcher to control the initial disturbance of rocket that provide new method and theory base and show the engineering system dynamic base on the multibody system transfer matrix method is effective.

本文以国防基础科研项目为背景,建立了通过控制定向器角运动来减小火箭弹起始扰动的多管火箭受控多体系统动力学模型,应用基于多体系统传递矩阵法的工程系统动力学理论,进行了定向器角度运动的影响因素分析,进行了受控多管火箭炮发射动力学和密集度数值仿真,得到了定向器俯仰和侧偏角控制参数对俯仰角和侧偏角的影响规律,为在火箭炮定向器上加装控制集成模块控制火箭弹的起始扰动和射击精度提供了新思路和理论基础,也表明了基于多体系统传递矩阵法的工程系统动力学理论的有效性。

Launch dynamics and transfer matrix method of multibody system are used to develop a launch dynamics model, equations of vibration characteristics and dynamic response. The firing dispersion test method of a non-full loading fire rocket based on the idea of equal initial disturbance is presented.

应用发射动力学和多体系统传递矩阵法理论,建立了多管火箭发射动力学模型,推导出了多管火箭振动特性和动力响应方程,形成了基于等起始扰动思想的多管火箭非满管射击密集度试验方法。

The launch site, testing system and ground application system have also been completed for launch.

在发射场上,测试系统与地面控制系统也完成了发射准备。

This paper, which focused on the structure optimization theory and method, has finished such studies as follows: The three dimension model has been built, which provide the necessary conditions for the building of the dynamics equivalent model. By the launch dynamics simulation, the loads of the key joints when the rocket is launched has been got, which provide the necessary data for the finite element analysis and the structure optimization. The finite element model of the excess weight parts of the rocket has been built, buy the finite element intension analysis of the model in two conditions, the displacement and the stress of the key points have been got, which make us know the distributing of the stress and the transmogrification of the part. To satisfy the intension and the precision design request and to decrease the weight of the part as many as possible, the part has been topology optimized by the structure optimization theory and method. After that, the new model has been analysis in structure and launch dynamics. The contrast of the character change of the old part and the new part and the influence on the rocket system have been studied.

本文以结构优化理论和方法为核心,主要做了以下工作:建立了某自行火箭炮全炮三维实体模型,为建立该火箭炮系统的动力学等效模型提供了必要条件,进行了发射动力学仿真,得到该火箭炮发射装置各关键连接部位在发射状态下的载荷,为有限元分析和结构优化提供了必需的数据;建立了该火箭炮发射装置超重部分的有限元模型,分两种工况,对模型进行了有限元强度分析,得出了关键部位的位移和应力值,对其的应力和变形分布有了具体的了解;运用结构优化的理论和方法,对该火箭炮发射装置超重部分进行了拓扑优化,使其在满足强度和精度的要求下尽可能多地减轻重量,对优化后得到的模型进行了结构分析和发射动力学分析,对比了该部件优化前后的特性变化以及对火箭炮系统的影响。

The "Launch Director", carrying his trusty tape-recorder, doing his walk-around of the rocket prior to launch.

"发射主管",进行他的可靠的磁带录音机,这样做,他步行绕的火箭在发射之前。

In this photo, a collection of the paraphernalia used to support a launch is visible -- the altiscope, landing locator, field equipment box, notepad, pre-launch checklist, and test equipment for setting the PET module.

在这照片,收集了有关用具,用于支持发射是有形-a ltiscope,登陆定位仪,野战装备中,记事本,发射前的清单,及测试设备设置宠物模块。

40 Zhuke established, the script deletes its files and their locationputs the files from version 2.17, its launch, close, delete the filesagain and again puts the files from version 2.40, test time, which willtime trials, the beetle will expire, close Player Hit icon and ascript, and then patiently waiting for some polminuty. At the end ofthe script window will appear with a request to launch a beetle, if you

自动翻译结果:在此脚本像蟒蛇那些谁使用液冷服Jukebox播放器,谁使用版本脚本2.40使审判永恒它是如何工作的:建立在2.40诸科,脚本删除其文件和它们所在的位置的文件从版本2.17 ,它的推出,关闭,删除的文件一再提出时间考验的文件从版本2.40,测试时间,将每一个重新运行,将过期的甲虫,关闭播放器点击图标和一个脚本,然后耐心地等待一些polminuty 。

"We are very pleased that the satellite is being shipped to the Baikonur launch base and we are looking forward to traveling to Kazakhstan for the August launch," said Peter Jackson, chief executive officer of AsiaSat."Our collaboration with Space Systems/Loral on this project has been very positive, and we expect to benefit from the company's long heritage of reliability in FSS satellites."

AsiaSat 5卫星基于劳拉太空系统公司的1300平台建造而成,携带了26台C波段和14台Ku波段转发器。C波段可扩展AsiaSat 2卫星的全亚洲覆盖范围,Ku波段覆盖范围包括三个高能光束,其中的两个光束将覆盖东亚和南亚,另外一个波束为在轨可控光束,能够定位并向卫星覆盖范围内的用户提供服务。

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