首页 | 本学科首页   官方微博 | 高级检索  
文章检索
  按 检索   检索词:      
出版年份:   被引次数:   他引次数: 提示:输入*表示无穷大
  收费全文   458篇
  免费   354篇
  国内免费   59篇
航空   454篇
航天技术   179篇
综合类   10篇
航天   228篇
  2024年   8篇
  2023年   15篇
  2022年   26篇
  2021年   45篇
  2020年   30篇
  2019年   24篇
  2018年   28篇
  2017年   18篇
  2016年   31篇
  2015年   17篇
  2014年   48篇
  2013年   39篇
  2012年   39篇
  2011年   42篇
  2010年   42篇
  2009年   29篇
  2008年   14篇
  2007年   50篇
  2006年   38篇
  2005年   34篇
  2004年   24篇
  2003年   19篇
  2002年   27篇
  2001年   24篇
  2000年   16篇
  1999年   22篇
  1998年   24篇
  1997年   20篇
  1996年   12篇
  1995年   16篇
  1994年   8篇
  1993年   10篇
  1992年   6篇
  1991年   6篇
  1990年   5篇
  1989年   3篇
  1988年   3篇
  1987年   9篇
排序方式: 共有871条查询结果,搜索用时 31 毫秒
191.
导弹级间热分离动态特性仿真研究   总被引:1,自引:0,他引:1  
任怀宇  张铎 《宇航学报》2005,26(4):509-513
级间热分离具有改善和提高继续飞行级的稳定性和入轨精度而被固体弹道式导弹广泛采用。以某导弹级间热分离为研究背景建立了分离动态方程,基于ADAMS平台进行了参数化模型的分离动力学仿真分析,协调、选择级间分离的各种参数,阐述了级间热分离需考虑的主要问题。研究表明,虚拟现实技术是实现合理选定导弹级间热分离时序的有效途径,不仅可提高分离系统设计、分析和校核过程中的条理化和清晰度,而且为实现分离系统设计与仿真的精确化、可视化、组合化和通用化提供了较好的基础。  相似文献   
192.
系统地介绍了复合固体推进剂玻璃转化温度(Tq)测试的几种表征方法,并评估了各方法的优良点。通过动态热机械分析(DMA)获得的推进剂参数曲线可以看出,用损耗模量E″的曲线表征Tq比较合适。  相似文献   
193.
薛光荣 《上海航天》2002,19(3):53-56
提出用一氧化二氮-乙炔火焰原子吸收光谱法测定热电池隔离粉中镁。介绍镁的最佳测定条件并具有良好线性范围的浓度,并对样品消化处理条件、干扰因素进行了综合考虑。该方法灵敏度高、重现性好,同时具有方法步骤简单、操作容易掌握等特点,达到了实验室分析质量控制的要求。  相似文献   
194.
任芬  吴光宗 《宇航学报》1996,17(4):14-19
本文对自适应发汗冷却(SCAT)弹头的热防护问题作了简化分析,并导得了热防护计算的简化计算公式。对铊,铟,锡和水四种冷却剂的情况,给出了算例。本文导行的公式,计算较简便,可作为弹头热防护设计的一种工程计算方法。这种工程计算方法亦可以用于地模拟实验前的予算。  相似文献   
195.
航天器热控系统中的热泵-蓄冷组合方案   总被引:3,自引:2,他引:3  
提出了旨在降低热控系统质量的热泵-蓄冷组合热控方案。通过对负荷进行预测,对热泵蓄冷系统的集成模式,系统的运行策略,以及蓄冷设备的容量等问题进行了分析。结果表明:通过合理优化系统的运行参数,热泵蓄冷组合方案能实现热控系统的轻量化设计要求,在未来航天热管理系统中具有相当的应用潜力。  相似文献   
196.
通过连续激光调制对薄板试样进行局部周期加热,采用红外扫描测温技术记录动态温度分布。利用博里叶变换分析温度基波相位和幅值变化,进而推算壁面的局部换热系数。介绍了该方法的测量原理,在风洞中对两种不同厚度的薄板进行了实验研究,并对实验结果进行了分析和讨论。  相似文献   
197.
热电偶响应对激光脉冲法测量热扩散率的影响   总被引:1,自引:0,他引:1  
用激光脉冲法测量热扩散率时,作为感温元件的热电偶总有一定的响应时间。试样达到最大温升的时间比较短时,热电偶响应时间所带来的测量误差就不能忽略不计。将热电偶处理为一阶测量环节,导出了考虑热电偶响应时间的试样背面温升表达式和修正关系曲线,并据此对实验结果进行修正。结果表明:经修正后的结果和文献[1]中提供的数据相吻合。  相似文献   
198.
空间核电源热管式辐射散热器热分析与参数优化   总被引:1,自引:0,他引:1       下载免费PDF全文
针对空间热管辐射散热器的特殊工况对散热器进行热分析建模,通过分析其传热原理,建立出热阻模型,并通过和实际设计进行对比,验证模型和计算方法的可行性。选取翅根温度、翅片长度和翅片厚度等参量作为约束条件,分别对热管式空间辐射散热器的翅片散热效率和系统质量特性进行优化分析,获得最优设计参数。  相似文献   
199.
TEGA, one of several instruments on board of the Phoenix Lander, performed differential scanning calorimetry and evolved gas analysis of soil samples and ice, collected from the surface and subsurface at a northern landing site on Mars. TEGA is a combination of a high temperature furnace and a mass spectrometer (MS) that was used to analyze samples delivered to the instrument via a robotic arm. The samples were heated at a programmed ramp rate up to 1000 °C. The power required for heating can be carefully and continuously monitored (scanning calorimetry). The evolved gases generated during the process can be analyzed with the evolved gas analyzer (a magnetic sector mass spectrometer) in order to determine the composition of gases released as a function of temperature. Our laboratory has developed a sample characterization method using a pyrolyzer integrated to a quadrupole mass spectrometer to support the interpretations of TEGA data. Here we examine the evolved gas properties of six types of hyperarid soils from the Pampas de La Joya in southern Peru (a possible analog to Mars), to which we have added with microorganisms (Salmonella typhimurium, Micrococcus luteus, and Candida albicans) in order to investigate the effect of the soil matrix on the TEGA response. Between 20 and 40 mg of soil, with or without ∼5 mg of lyophilized microorganism biomass (dry weight), were placed in the pyrolyzer and heated from room temperature to 1200 °C in 1 h at a heating rate of 20 °C/min. The volatiles released were transferred to a MS using helium as a carrier gas. The quadrupole MS was ran in scan mode from 10 to 200 m/z. In addition, ∼20 mg of each microorganism without a soil matrix were analyzed. As expected, there were significant differences in the gases released from microorganism samples with or without a soil matrix, under similar heating conditions. Furthermore, samples from the most arid environments had significant differences compared with less arid soils. Organic carbon released in the form of CO2 (ion 44 m/z) from microorganisms evolved at temperatures of ∼326.0 ± 19.5 °C, showing characteristic patterns for each one. Others ions such as 41, 78 and 91 m/z were also found. Interestingly, during the thermal process, the release of CO2 increased and ions previously found disappeared, demonstrating a high-oxidant activity in the soil matrix when it was subjected to high temperature. Finally, samples of soil show CO2 evolved up to 650 °C consistent with thermal decomposition of carbonates. These results indicate that organics mixed with these hyperarid soils are oxidized to CO2. Our results suggest the existence of at least two types of oxidants in these soils, a thermolabile oxidant which is highly oxidative and other thermostable oxidant which has a minor oxidative activity and that survives the heat-treatment. Furthermore, we find that the interaction of biomass added to soil samples gives a different set of breakdown gases than organics resident in the soil. The nature of oxidant(s) present in the soils from Pampas de La Joya is still unknown.  相似文献   
200.
The ability to achieve long-endurance station-keeping flights makes stratospheric airships desirable platforms for the provision of communication and surveillance services. To maintain long-endurance flights, it is necessary to consider the problem of energy consumption. In this paper, we discuss long-endurance flight scenarios of stratospheric airships in the presence of thermal effects. The balance between buoyancy and gravity is influenced by thermal effects during the diurnal cycle. We perform a theoretical analysis based on the helium’s mass, pressure differential, and altitude as the main factors. To verify the effectiveness of the control over the pressure differential and the altitude, three long-endurance flight scenarios are proposed and compared. Then, the corresponding optimization problems are constructed to determine the energy-minimum flight. Finally, further efforts are made to reduce energy consumption. The realization and limitations of two strategies for improvement are analyzed. A comparison with other scenarios shows the effectiveness of energy conservation. The study in this paper thus provides a reference for station-keeping applications of stratospheric airships.  相似文献   
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号