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A small, vibration- and shock-resistant thermoluminescent dosemeter /TLD/ system--named PILLE--was developed at the Health Physics Department of the Central Research Institute for Physics, Budapest, to measure the cosmic radiation dose on board orbital stations. The first on-board measurements with this system were performed /by B. Farkas, the Hungarian astronaut/, on the Salyut-6 space station in 1980. The same instrument was used by other crews in the following years. Doses measured at different sites in Salyut-6 are presented. The dose rates varied from 0.07 to 0.11 mGy.day-1. After the first cosmic measurements, the system was further developed. The minimum detectable dose of the new TLD system is 1 microGy, i.e. less by on order of magnitude than that of the former system. The self-irradiation dose rate of the TLD bulbs is also reduced--by more than one order of magnitude--to 10 nGy.h-1, by the use of potassium-free glass for the bulb envelope. This new type of PILLE TLD system is currently on-board Salyut-7. The dose rates /0.12-0.23 mGy.day-1/ measured in 1983 are presented in detail.  相似文献   
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The VEGA-1 and VEGA-2 spacecraft made their closest approach to Comet Halley on 6 and 9 March, respectively. In this paper those results of the onboard imaging experiment which were obtained around closest approach are discussed. The nucleus of the comet was clearly identifiable as an irregularly shaped object, with overall dimensions of (16±1)×(8±1)×(8±1) km. The nucleus rotates in the prograde sense about an axis nearly perpendicular to the orbital plane with a period of 53±2 hours. Its albedo is only 0.04±0.020.01 Many of the jet features observed during the second fly-by have been spatially reconstructed. Their sources form a quasi-linear structure on the surface. The dust above the surface is shown to be generally optically thin with the exception of certain specific dust jets. Brightness features on the surface are clearly seen. Correlating our data with other measurements, we conclude that the dirty snow-ball model will probably need to be revised.  相似文献   
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The magnetometer on the STEREO mission is one of the sensors in the IMPACT instrument suite. A single, triaxial, wide-range, low-power and noise fluxgate magnetometer of traditional design—and reduced volume configuration—has been implemented in each spacecraft. The sensors are mounted on the IMPACT telescoping booms at a distance of ~3 m from the spacecraft body to reduce magnetic contamination. The electronics have been designed as an integral part of the IMPACT Data Processing Unit, sharing a common power converter and data/command interfaces. The instruments cover the range ±65,536 nT in two intervals controlled by the IDPU (±512 nT; ±65,536 nT). This very wide range allows operation of the instruments during all phases of the mission, including Earth flybys as well as during spacecraft test and integration in the geomagnetic field. The primary STEREO/IMPACT science objectives addressed by the magnetometer are the study of the interplanetary magnetic field (IMF), its response to solar activity, and its relationship to solar wind structure. The instruments were powered on and the booms deployed on November 1, 2006, seven days after the spacecraft were launched, and are operating nominally. A magnetic cleanliness program was implemented to minimize variable spacecraft fields and to ensure that the static spacecraft-generated magnetic field does not interfere with the measurements.  相似文献   
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At 1 AU in 1998, when solar activity was increasing, the distribution of hour averages of the solar wind speed was approximately lognormal. There was no distinct separation between fast and slow flows. The density, temperature and magnetic field strength also had lognormal distributions. It was possible to identify distinct structures such as corotating streams and magnetic clouds during some intervals. We suggest that coexistence of a simple statistical structure and deterministic physical structures is the consequence of the dynamical evolution and interactions of the flows between the sun and 1 AU and a relatively complex source signal. This revised version was published online in June 2006 with corrections to the Cover Date.  相似文献   
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During the last years data have evidenced that alteration in nucleic acid metabolism, expecially increased urinary excretion of modified nucleosides reflects physiological changes in living organism. In relation with the Soyuz-36-Salyut-6-Soyuz-35 mission in 1980 urinary nucleoside excretion of two astronauts /B.F., V.K./ were traced. Individual daily urine samples were collected for 4 days before starting and 6 days after landing and were analysed with improved analytical procedures /affinity chromatography, high Performance liquid chromatography/. Levels of 1-methylinosine, 1-methylguanosine and N,2,2-dimethylguanosine in urine were determined. Thus recorded changes differ considerably at two astronauts. One of the /V.K./ excreted nucleosides normally, another /B.F./ showed increase to 200-400 % levels excretion of above nucleosides on the second day after landing. The peak values disappeared on the 3-6 days after. To interpret this phenomenon extreme factors of space-flight /weightlessness, stress, radiations, etc./ have to be taken into consideration. However, we attach importance to training of astronauts. During the last decade data have evidenced that alterations in the metabolism of nucleic acids especial increased urinary excretion of modified nucleosides reflects physiological and in some cases pathological changes in living organism. In relation with the Soyuz-36-Salyut-6-Soyuz 35 mission urinary excretion of certain modified nucleosides of two astronauts /B.F. and V.K./ were measured. The aim of the measurements was: how the metabolism of transfer ribonucleic acids /tRNAs/ referring to cosmic flight, how it is reflected in urinary excretions of modified nucleosides. For these purposes we studied the excretion of methylguanosine, dimethylguanosine and methylinosine. These nucleosides are the normal minor components of tRNA.  相似文献   
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Verigin  M.I.  Slavin  J.  Szabo  A.  Kotova  G.A.  Remizov  A.P.  Rosenbauer  H.  Livi  S.  Szegö  K.  Tátrallyay  M.  Schwingenschuh  K.  Zhang  T.-L. 《Space Science Reviews》2004,111(1-2):233-243
Detailed analysis of disturbances observed on 24 March, 1989 far upstream of the usual Martian bow shock position was completed with the use of the planetary obstacle and bow shock models relevant for the period of Phobos 2 observations and for low Mach numbers, respectively. It is proven that the system of discontinuities observed in the solar wind between 18:42 and 19:36 UT was the consequence of unusually distant planetary bow shock excursions. The cause was unusually small ρV 2 and M a values in the solar wind flow.  相似文献   
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