全文获取类型
收费全文 | 251篇 |
免费 | 44篇 |
国内免费 | 7篇 |
专业分类
航空 | 21篇 |
航天技术 | 140篇 |
航天 | 141篇 |
出版年
2024年 | 3篇 |
2023年 | 9篇 |
2022年 | 12篇 |
2021年 | 8篇 |
2020年 | 6篇 |
2019年 | 8篇 |
2018年 | 10篇 |
2017年 | 2篇 |
2016年 | 4篇 |
2015年 | 9篇 |
2014年 | 31篇 |
2013年 | 19篇 |
2012年 | 15篇 |
2011年 | 26篇 |
2010年 | 18篇 |
2009年 | 14篇 |
2008年 | 31篇 |
2007年 | 14篇 |
2006年 | 12篇 |
2005年 | 13篇 |
2004年 | 9篇 |
2003年 | 6篇 |
2002年 | 5篇 |
2001年 | 1篇 |
2000年 | 8篇 |
1999年 | 1篇 |
1998年 | 4篇 |
1997年 | 3篇 |
1996年 | 1篇 |
排序方式: 共有302条查询结果,搜索用时 359 毫秒
271.
T. Hashimoto T. HoshinoS. Tanaka H. OtakeM. Otsuki S. WakabayashiH. Morimoto K. Masuda 《Acta Astronautica》2014
The Japan Aerospace Exploration Agency (JAXA) views the lunar lander SELENE-2 as the successor to the SELENE mission. In this presentation, the mission objectives of SELENE-2 are shown together with the present design status of the spacecraft. JAXA launched the Kaguya (SELENE) lunar orbiter in September 2007, and the spacecraft observed the Moon and a couple of small satellites using 15 instruments. As the next step in lunar exploration, the lunar lander SELENE-2 is being considered. SELENE-2 will land on the lunar surface and perform in-situ scientific observations, environmental investigations, and research for future lunar utilization including human activity. At the same time, it will demonstrate key technologies for lunar and planetary exploration such as precise and safe landing, surface mobility, and overnight survival. The lander will carry laser altimeters, image sensors, and landing radars for precise and safe landing. Landing legs and a precisely controlled propulsion system will also be developed. A rover is being designed to be able to travel over a wide area and observe featured terrain using scientific instruments. Since some of the instruments require long-term observation on the lunar surface, technology for night survival over more than 2 weeks needs to be considered. The SELENE-2 technologies are expected to be one of the stepping stones towards future Japanese human activities on the moon and to expand the possibilities for deep space science. 相似文献
272.
273.
274.
为提高月球着陆器着陆可靠性,需识别潜在的故障模式对稳定性着陆带来的影响。建立了着陆器的动力学模型,给出了着陆器着陆时的七种极限工况,作为故障模式分析的基础;针对动力下降段三种典型故障模式,即主发动机延时关机、储箱残留液体着陆和触月信号延迟发出,建立与延时关机对应的上抛、平抛运动和数学关系,与残留液体着陆等效的单摆模型,施加触月信号延迟发出所产生的推力曲线,利用Adams软件进行动力学仿真;结果表明储箱残留液体着陆影响较小,另外两种故障模式使着陆时抗倾倒性能和缓冲性能恶化,增加着陆不稳定性。 相似文献
275.
276.
Jonathan G. Metts 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2012,49(1):204-212
Thermal control of a space suit during extravehicular activity (EVA) is typically accomplished by sublimating water to provide system cooling. Spacecraft, on the other hand, primarily rely on radiators to dissipate heat. Integrating a radiator into a space suit has been proposed as an alternative design that does not require mass consumption for heat transfer. While providing cooling without water loss offers potential benefits for EVA application, it is not currently practical to rely on a directional, fixed-emissivity radiator to maintain thermal equilibrium of a spacesuit where the radiator orientation, environmental temperature, and crew member metabolic heat load fluctuate unpredictably. One approach that might make this feasible, however, is the use of electrochromic devices that are capable of infrared emissivity modulation and can be actively controlled across the entire suit surface to regulate net heat flux for the system. Integrating these devices onto the irregular, compliant space suit material requires that they be fabricated on a flexible substrate, such as Kapton film. An initial assessment of whether or not this candidate technology presents a feasible design option was conducted by first characterizing the mass of water loss from sublimation that could theoretically be saved if an electrochromic suit radiator was employed for thermal control. This is particularly important for lunar surface exploration, where the expense of transporting water from Earth is excessive, but the technology is potentially beneficial for other space missions as well. In order to define a baseline for this analysis by comparison to actual data, historical documents from the Apollo missions were mined for comprehensive, detailed metabolic data from each lunar surface outing, and related data from NASA’s more recent “Advanced Lunar Walkback” tests were also analyzed. This metabolic database was then used to validate estimates for sublimator water consumption during surface EVAs, and solar elevation angles were added to predict the performance of an electrochromic space suit radiator under Apollo conditions. Then, using these actual data sets, the hypothetical water mass savings that would be expected had this technology been employed were calculated. The results indicate that electrochromic suit radiators would have reduced sublimator water consumption by 69.0% across the entire Apollo program, for a total mass savings of 68.5 kg to the lunar surface. Further analysis is needed to determine the net impact as a function of the complete system, taking into account both suit components and consumable mass, but the water mass reduction found in this study suggests a favorable system trade is likely. 相似文献
277.
针对月球探测器定点着陆任务的需要,研究了基于三维地形匹配的导航方法。对三维地形匹配问题,将高程方差图局部极值点作为三维地形特征,在构建地形特征之间的相对位置与角度不变量的基础上,提出了基于投票的三维地形匹配策略。针对测量噪声统计特性的不确定性,将Sage\|Husa噪声估计算子与迭代卡尔曼滤波相结合,通过对测量噪声进行在线估计有效避免滤波精度下降甚至滤波发散的出现。数字仿真结果表明所研究的导航方法能够有效地实现探测器相对位置和姿态的精确估计。 相似文献
278.
L.K. Amekudzi A. Bracher K. Bramstedt A. Rozanov H. Bovensmann J.P. Burrows 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2008,41(11):1921-1932
Vertical profiles of stratospheric nitrogen dioxide (NO2) have been retrieved from moderate resolution lunar occultation transmission spectra measured by Scanning Imaging Absorption spectroMeter for Atmospheric CHartographY (SCIAMACHY) on board the European Environmental Satellite (ENVISAT). These measurements were taken over the high southern latitude of 50°–90° during the period of 2003–2005. To assess the accuracy of the retrieved NO2 profiles, the SCIAMACHY nighttime NO2 profiles were compared with NO2 profiles retrieved from sunrise solar occultation spectra measured by the Halogen Occultation Experiment (HALOE) and the Stratospheric Aerosol and Gas Experiments II (SAGE II) using a photochemical correction model. The validation results show good agreement of SCIAMACHY lunar occultation NO2 with scaled HALOE and SAGE II profiles. The relative mean differences (rmd) with scaled HALOE profiles are within −13% to +5% and standard deviations (rms) of the relative differences are within 3–19% between 25 and 38 km. The rmd and rms with scaled SAGE II NO2 profiles are in the range of −9 to +7 and 10–17% respectively between 22 and 39 km. 相似文献
279.
In this paper,technological progress for China's microwave remote sensing is intro-duced.New developments of the microwave remote sensing instruments for meteorological satellite FY-3,ocean dynamic measurement satellite(HY-2),environment small SAR satellite(HJ-1C) and China's lunar exploration satellite(Chang'E-1),geostationary orbit meteorological satellite FY-4M,are reported. 相似文献
280.
N. Hasebe N. Yamashita O. Okudaira S. Kobayashi H. Yamamoto T. Ishizaki K. Hirano K. Sakurai T. Miyachi M. Miyajima M. Fujii M.-N. Kobayashi T. Takashima E. Shibamura O. Gasnault S. Maurice C. d’Uston R. Reedy M. Grande 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2008
The high precision gamma-ray spectrometer (GRS) is scheduled to be launched on the lunar polar orbiter of the SELENE mission in 2007. The GRS consists of a large Ge crystal as a main detector and massive bismuth germanate crystals as an anticoincidence detector. A Stirling cryocooler was adopted in cooling the Ge detector. The flight model of SELENE GRS has been completed and an energy resolution of 3.0 keV (FWHM) at 1.332 MeV has been achieved. The spectrometer aims to observe nuclear line gamma rays emitted from the lunar surface in a wide energy range from 100 keV to 12 MeV for one year and more to obtain chemical composition on the entire lunar surface. The gamma-ray data enable us to study lunar geoscience problems including crust and mantle composition, and volatile reservoirs at polar regions. 相似文献