共查询到20条相似文献,搜索用时 125 毫秒
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介绍一种安装在E-9A飞机上的大型遥测相控阵天线系统的技术要求、设计与制造方法以及外场试验结果,并对天线系统的组成和其中的关键部件作了较详细的说明.生产的两套天线已成功地用于海湾靶场上的空空导弹试验,它具有独立捕获、跟踪5发遥测弹的能力. 相似文献
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西德的微重力试验回收舱——信使(SPACE COURIER)是一种低成本再入飞行器,它能携带若干个航天试验性载荷,可用长征2号、阿里安和其它运载系统发射,具有很大的潜在商业市场,计划于1992年底进行首次飞行。本文介绍了信使回收舱的任务,系统和分系统设计及其有效载荷。 相似文献
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I. A. Babushkin G. P. Bogatyrev A. F. Glukhov G. F. Putin S. V. Avdeev A. I. Ivanov M. M. Maksimova 《Cosmic Research》2001,39(2):150-158
The DACON instrument for studying the convection caused by low frequency microaccelerations aboard spacecraft is described. The convection sensor serves as a measuring element of this instrument. This is a cylindrical cavity filled with air, where two crossed differential thermocouples are located. The thermocouple junctions lay on two mutually perpendicular lines parallel to the bases of the cylinder and crossing at its axis. The distances from the junctions to this axis are equal. The lateral surface of the cylinder is thermally insulated, the difference of temperatures on its bases being kept constant. One of the tasks for the sensor is to prepare the data for checking the adequacy of mathematical models of fluid convection under weightlessness conditions and for obtaining quantitative characteristics of the microgravitational medium. The results of ground-based tests of the DACON instrument and the results of experiments with it aboard the Mirstation are presented. 相似文献
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《Acta Astronautica》1987,15(8):561-565
The stability of long liquid bridges under non-axisymmetric disturbances like a microgravitational force acting perpendicular to the liquid bridge axis or a non-coaxiality of the disks is analyzed through an asymptotic method based on bifurcation techniques. Results obtained indicate that such non-axisymmetric effects are of higher order than those produced by axisymmetric perturbations. 相似文献
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A number of scientific and technical experiments were carried out and are still being carried out onboard the Mirorbital station in various fields: physics of fluids, space materials study, astrophysics, biotechnology, and so on. The quality and reliability of space experiments are essentially dependent on a knowledge of real microgravitational situation onboard a satellite, which essentially depends on vibrational perturbations. A lot of vibration processes studies have been done up to now on the Mirstation in the following lines of research: control of dynamic and exploitation regimes when carrying out biotechnological and technological experiments; determination of the contribution of different onboard systems and mechanisms to the total vibration perturbations power; and investigation of distributions of microacceleration levels and dynamics of vibration processes in different modules and segments of the orbital station. This paper presents the results of the analysis of vibration perturbations produced by some standard onboard Mirstation systems in a configuration when the KVANT-2 and KRISTALL modules were arranged along the yaw axis of the mainframe. It is shown that due to strong requirements for tolerable levels of the microaccelerations onboard the International Space Station (ISS), the investigations of microgravitational situation, as an integral part of the technological environment, now have a high priority. 相似文献
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Henderson IW 《Journal of the British Interplanetary Society》1989,42(7):363-366
Under conditions of microgravity severe alterations in body fluid composition and volume take place largely as a result of "cardiothoracic pooling" or headward shift of blood. Inappropriate endocrine, renal and cardiovascular responses result from the "misreading" of homeostatic signals by physiological receptors to produce an as yet incompletely defined syndrome under microgravitational conditions. 相似文献
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文章介绍了美国X—38计划及其翼伞返回系统的概况,分析了历次空投试验翼伞返回系统的状况、工作过程、出现的反翘现象等。 相似文献
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The mode of monoaxial solar orientation of a designed artificial Earth satellite (AES), intended for microgravitational investigations, is studied. In this mode the normal line to the plane of satellite’s solar batteries is permanently directed at the Sun, the absolute angular velocity of a satellite is virtually equal to zero. The mode is implemented by means of an electromechanical system of powered flywheels or gyrodynes. The calculation of the level of microaccelerations arising on board in such a mode, was carried out by mathematical modeling of satellite motion with respect to the center of masses under an effect of gravitational and restoring aerodynamic moments, as well as of the moment produced by the gyrosystem. Two versions of a law for controlling the characteristic angular momentum of a gyrosystem are considered. The first version provides only attenuation of satellite’s perturbed motion in the vicinity of the position of rest with the required velocity. The second version restricts, in addition, the increase in the accumulated angular momentum of a gyrosystem by controlling the angle of rotation of the satellite around the normal to the light-sensitive side of the solar batteries. Both control law versions are shown to maintain the monoaxial orientation mode to a required accuracy and provide a very low level of quasistatic microaccelerations on board the satellite. 相似文献
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载人飞船的开伞控制方案是回收着陆系统设计中的一个关键环节,它直接关系到飞船回收着陆系统工作的成败。文章根据载人飞船特点的分析,制订了飞船开伞控制方案,即采用静压高度控制法来控制开伞,然后根据静压高度控制的工作原理,详细介绍了开伞控制方案的设计方法和流程。仿真试验和飞行试验结果表明:"神舟号"载人飞船开伞控制方案的设计是合理的、正确的。 相似文献
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文章主要介绍了载人飞船回收着陆分系统可靠性、安全性设计准则、设计分析方法、设计措施以及试验验证等。地面试验以及飞行试验的验证表明:回收着陆分系统的可靠性、安全性设计措施有效,试验验证充分,分系统的工作可靠,可靠性和安全性均满足其指标要求。 相似文献
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月球取样返回器回收半实物仿真系统是通过模拟返回器取压孔附近压力环境,将回收程控装置硬件实物接入仿真系统并构成实时仿真回路的半实物仿真平台。文章介绍了月球取样返回器回收半实物仿真系统的研制意义,对系统总体结构和设计方案、网络环境、运行流程和新的设计特点进行概括,在面向对象的基础上建立了分阶段的月球取样返回器降落伞回收系统整个工作过程的动力学模型,利用空投试验测量数据对模型的仿真精度进行验证分析,并对半实物仿真系统的实时性和压力模拟精度进行了分析。结果表明,半实物仿真系统的各项技术参数均达到设计指标,可为中国探月工程三期中月球取样返回器回收分系统的可靠性评估提供重要的技术支持。 相似文献
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This paper presents the review of results of the navigating experiments which have been carried out during flight of microgravitational space platform (MSP) Foton-M2 in May–June 2005. The brief characteristic of the created MIRAGE–M equipment consisting from magnitometric system and satellite radionavigation receiver is given. The measurements have allowed to restore unguided MSP movement and to estimate a level of microaccelerations (microgravitations) onboard during flight, and have provided precision time-position binding of the research experiments. The data from the equipments transmitted on the telemetering channel have allowed testing the information technologies of virtual support of experiments in space. Flight testing of the equipment has allowed make a conclusion on usefulness of accommodation onboard the small-sized auxiliary navigating system focused for work with users of research experiments. The experiments on MSP Foton-M2 are the development of experiments with MIRAGE equipment carried out in 1999 during flight time of MSP Foton-12 [N.D. Semkin, V.V. Ivanov, V.I. Abrushkin, V.L. Balakin, I.V. Belokonov, K.E. Voronov, The experiments with magnetic fields formed by technical equipment inside Foton-12 spacecraft: the results of the MIRAGE experiments, in: Proceedings of International Conference “Scientific and Technological Experiments on Russian Foton/Bion Recoverable Satellites: Results, Problems and Outlooks”, 25–30 June 2000, pp. 116–122; V.L. Balakin, I.V. Belokonov, V.V. Ivanov, “Determination of motion of spacecraft Foton-12 as a result of magnetic fields measurement in MIRAGE experiment”, pp. 231–238 (published in the same place)].Paper is executed within the framework of the grant of the Russian Fund of Fundamental Researches 06-08-00244. 相似文献