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排序方式: 共有258条查询结果,搜索用时 375 毫秒
251.
E. Grün E. Bussoletti A. Minafra H. Kuczera J.A.M. McDonell 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》1984,4(9):291-295
The IPM detector consists of two separate impact ionization detectors, one of them covered by a 2.5 μm thick plastic film and a piezoelectric sensor mounted to the back of the joint impact plate. First impact tests, with iron projectiles in the mass range 10?15 to 10?9 g and in the speed range 1 km/s to 70 km/s, were performed with the calibration (FS) and the flight (F) model of this detector. The charge yield at 69 km/s impact speed (flyby speed of GIOTTO) has been extrapolated from the data and amounts to 400 Coulombs per gram. This corresponds to a preliminary sensitivity threshold for the impact ionization detector of about 6×10?17 g. The penetration limit introduced by the plastic film is about 10?14 g for iron particles. Only the biggest particles used for the test produced signals at the piezoelectric sensor. If one assumes an energy dependence of the piozoelectric signal, a preliminary sensitivity threshold of about 10?13 g at 69 km/s can be established. 相似文献
252.
D. Spänkuch W. Döhler J. Güldner 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》1981,1(4):239-243
Based on measurements with the interferometer spectrometer SI-1 on board of Meteor satellites the following problems are investigated: the systematic effect of the spectral response function in deriving effective radiation temperatures; the selection of ‘optimal’ spectral channels within the 15 μm region, and effects of additional molecular absorbers on the determination of the temperature profile. It can be shown that using broad-band window channels (half width ?20cm?1) the derived surface temperature is significantly different from the surface temperature derived from narrow spectral band channels (e.g. for the HIRS window channel 8 this difference is about 1° C). Simulations of some combinations of spectral channels including one proposed as an optimal approach show no significant difference in the derived temperature profile. Neglecting the ozone absorption of the 14.1 μm band leads to a change in radiance of about 1.5 mW/m2sr cm?1 and to a systematic error of the derived temperature of about ?2° C in the troposphere. 相似文献
253.
B. Heber E. Keppler R.G. Marsden C. Tranquille B. Blake M. Fränz 《Space Science Reviews》2001,97(1-4):363-366
Moraal and Steenberg (1999), showed that the peak energy in the anomalous cosmic ray spectra is independent of the radial
distance up to a few AU away from the termination shock but dependent on the solar wind speed, the radius of the termination
shock and the scattering strength. In this paper we will discuss the variation of the cosmic ray oxygen energy spectrum as
measured by the Ulysses EPAC and the COSPIN/LET on board Ulysses. We found that the peak energy decreased from ∼5 MeV nucl−1, when Ulysses was at high northern heliographic latitudes embedded in the fast solar wind to ∼3.5 MeV n−1, in the streamer belt. The shift towards lower energy might also be caused by changing modulation although Voyager measurements
indicate no variation of the ACR Oxygen spectrum at ∼60 AU.
This revised version was published online in August 2006 with corrections to the Cover Date. 相似文献
254.
T. Tänczer Gy.Cs. Hegedüs 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》1981,1(4):327-330
An attempt for digital processing of analog images taken in the infrared channel (10.5–11.5 μm) from TIROS-N is presented. The data digitized to 8-bits are normalized by using SR Data Manipulator. The investigated period is November 3–4, 1979. The geographic rectification moves the data into a polar stereographic map. To estimate the cloud heights empirical relationships are applied. The following characteristics of the cloud field are produced: the cloud amount, the dominant cloud-type, the daily variation of IR brightness temperature and the cloud texture. The results are visualized on a colour display. 相似文献
255.
256.
D. Müller 《Space Science Reviews》2001,99(1-4):105-116
We briefly review the available data on cosmic rays beyond the `knee, i.e., over the energy range from 1015 to more than 1020 eV. We discuss the observational status of the field, review some of the current attempts to explain the origin of these particles, and briefly survey the prospects of future measurements. 相似文献
257.
The linear shaped charge cutting technology is an effective technology for aircraft separation. It can separate invalid components from aircrafts timely to achieve light-weight. Magnesium alloy is the lightest metal material, and can be used to cast effective light-weight components of an aircraft construction. However, the application study of the linear shaped charge cutting technology on magnesium alloy components is basically blank. In response to the demand for the linear separation of magnesium alloys, the Mg-12Gd-0.5Y-0.4Zn alloy is selected to carry out the target shaped charge cutting test. The effects of the shaped charge line density, cutting thickness, and mechanical properties on the cutting performance of the alloy are studied. The shaped charge cutting mechanism is analyzed through the notch structure. The results show that the linear shaped charge cutting performance is significantly affected by the penetration and the collapse. The higher the linear density is, the stronger the ability of the linear shaped charge cutter is, and the greater the penetration depth is, which is advantageous. However, the target structure will be damaged when it is too large (e.g., 4.5 g?m-1). Within 12 mm, when the cutting thickness of the target increases, the penetration depth increases. The lower the tensile strength is, the greater the penetration depth is, and the more conducive the penetration depth to the shaped charge cutting is. When the elongation (EL) increases to 12%, the collapse of the target is incomplete and the target cannot be separated. When the tensile strength of the Mg-Gd-Y-Zn alloy is less than 350 MPa, the EL is less than 6.5%, the cutting thickness is less than 12 mm, and the linear shaped charge cutting of the magnesium alloy can be achieved stably. 相似文献
258.
对巨磁电阻材料La1-xZnxMnO3(x=0.1,0.3,0.5,0.7,0.9,1.0)样品的制备工艺、晶体结构、微观结构进行研究。结果表明,样品ZnO与MnO2固相反应的烧结温度和时间分别大于1300℃和6h时,反应生成具有四面体结构的ZnMnO3化合物;压制成型的压力对结构具有一定影响;不同浓度的Zn2 (x=0.1,0.3,0.5,0.7,0.9)掺杂样品在1350℃烧结12h后,均具有钙钛矿结构,但掺杂浓度在大于x=0.5时有新的衍射峰,产生新的物相,从而影响巨磁电阻效应性能。 相似文献