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951.
Pratt G. W. Arnaud M. Biviano A. Eckert D. Ettori S. Nagai D. Okabe N. Reiprich T. H. 《Space Science Reviews》2019,215(2):1-19
Space Science Reviews - The QB50 mission is a satellite constellation designed to carry out measurements at between 200–380 km altitude in the ionosphere. The multi-needle Langmuir probe... 相似文献
952.
M. O. Riazantseva O. V. Khabarova G. N. Zastenker J. D. Richardson 《Cosmic Research》2005,43(3):157-164
This work is devoted to studying the sharp boundaries of small-scale structures of the solar wind according to the data of measurements with high time resolution onboard the INTERBALL-1 satellite and simultaneous measurements of the WIND spacecraft. Such issues as the character of change of various plasma and magnetic field parameters on these boundaries, the duration of boundary passage and the balance of the total (thermal plus magnetic) pressure on the boundaries of the structures are considered. On the basis of the vast statistical material available, the typical conditions in the solar wind are investigated, in which such sharp boundaries are observed.__________Translated from Kosmicheskie Issledovaniya, Vol. 43, No. 3, 2005, pp. 163–170.Original Russian Text Copyright © 2005 by Riazantseva, Khabarova, Zastenker, Richardson. 相似文献
953.
Influence of clinorotation and fettering stress on tail regeneration of Triturus vulgaris (Urodela).
H J Anton E N Grigoryan K Krupp-Beyerlein H Pitzer V I Mitashov 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》1998,21(8-9):1159-1162
Tail-amputated adult Triturus vulgaris, fettered in cuvettes of a fast-rotating clinostat were exposed to simulated weightlessness (60 rpm; equiv. to 10(-3)-10(-4) g), during a 14-day period. To feed and clean the animals rotation was stopped once a day for approx. 10 min. To test the influence of the fettering stress, a second series of animals was kept separately under normal earth conditions without rotation. A further control series was kept in a dark container without any handicap. While tail regeneration of the rotated animals was markedly accelerated, the fettered-only animals showed a considerably less marked acceleration effect. At the end of the 14-day period, all regenerates were reamputated together with an additional 5 mm of the tail stump. Although this second level of amputation was distant from the first, the regenerative growth rate of the rotated series was accelerated 123% in contrast to both the control and the fettered-only series. Our results demonstrate that the growth acceleration is induced by clinorotation. Fettering stress has no comparable influence. The growth promoting effect is not limited to the regenerating area. 相似文献
954.
F.E. Bauer C. Vignali D.M. Alexander W.N. Brandt G.P. Garmire A.E. Hornschemeier P.S. Broos L.K. Townsley D.P. Schneider 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2004,34(12):2555-2560
We investigate the nature of the faint X-ray source population through X-ray spectroscopy and variability analyses of 136 active galactic nuclei (AGN) detected in the 2 Ms Chandra Deep Field-North Survey with >200 background-subtracted 0.5–8.0 keV counts [F0.5–8.0 keV = (1.4−200) × 10−15 erg cm−2 s−1]. Our preliminary spectral analyses yield median spectral parameters of Γ = 1.61 and intrinsic NH = 6.2 × 1021 cm−2 (z = 1 assumed when no redshift available) when the AGN spectra are fitted with a simple absorbed power-law model. However, considerable spectral complexity is apparent (e.g., reflection, partial covering) and must be taken into account to model the data accurately. Moreover, the choice of spectral model (i.e., free vs. fixed photon index) has a pronounced effect on the derived JVH distribution and, to a lesser extent, the X-ray luminosity distribution. We also find that among the 136 AGN, 10 (≈7%) show significant Fe K emission-line features with equivalent widths in the range 0.1–1.3 keV. Two of these emission-line AGN could potentially be Compton thick (i.e., Γ < 1.0 and large Fe K equivalent width). Finally, we find that 81 (≈60%) of the 136 AGN show signs of variability, and that this fraction increases significantly (≈80–90%) when better photon statistics are available. 相似文献
955.
THE DIGITAL WAVE-PROCESSING EXPERIMENT ON CLUSTER 总被引:1,自引:0,他引:1
L. J. C. Woolliscroft H. St. C. Alleyne C. M. Dunford A. Sumner J. A. Thompson S. N. Walker K. H. Yearby A. Buckley S. Chapman M. P. Gough 《Space Science Reviews》1997,79(1-2):209-231
The wide variety of geophysical plasmas that will be investigated by the Cluster mission contain waves with a frequency range from DC to over 100 kHz with both magnetic and electric components. The characteristic duration of these waves extends from a few milliseconds to minutes and a dynamic range of over 90 dB is desired. All of these factors make it essential that the on-board control system for the Wave-Experiment Consortium (WEC) instruments be flexible so as to make effective use of the limited spacecraft resources of power and telemetry-information bandwidth. The Digital Wave Processing Experiment, (DWP), will be flown on Cluster satellites as a component of the WEC. DWP will coordinate WEC measurements as well as perform particle correlations in order to permit the direct study of wave/particle interactions. The DWP instrument employs a novel architecture based on the use of transputers with parallel processing and re-allocatable tasks to provide a high-reliability system. Members of the DWP team are also providing sophisticated electrical ground support equipment, for use during development and testing by the WEC. This is described further in Pedersen et al. (this issue). 相似文献
956.
The equations of the mathematical model are solved in terms of special functions. The results for the design scheme of the aircraft forebody are obtained with a guaranteed accuracy by the stable method of functional normalization. 相似文献
957.
新型封严涂层高温高速磨耗试验机的研制 总被引:1,自引:0,他引:1
为模拟航空涡轮发动机气路封严配副在工作状态下的磨损磨耗现象,研究封严涂层的可磨耗性能,研制了1套新型的可磨耗性能评价试验器。该试验器采用叶片-涂层刮削式磨耗副,使用模拟轮盘带动叶片高速旋转实现叶尖的切线速度;采用封严涂层试样径向进给以模拟叶片刮削切入;使用压电石英晶体3向测力仪定量测量瞬态刮削力;采用高速高温火焰加热试样。考核结果表明:试验器能够完成叶尖切线速度为0~300 m/s、进给速率为1.5~2025μm/s、加热温度为20~800℃条件下的磨耗试验,试验效果良好,数据稳定可靠。 相似文献
958.
V. N. Oraevskii S. N. Kuznetsov V. V. Malyshev V. E. Usachov Yu. D. Tychinskii 《Cosmic Research》2004,42(1):23-31
We study a possibility of observing the eclipses of the Sun by the Moon from satellite orbits. The scientific tasks planned to be solved onboard satellites are considered. The requirements for the observation of eclipses and for the appropriate satellite trajectories are formulated. A technique of the analysis and synthesis of such trajectories is developed, and some results of preliminary ballistic studies are presented. These results confirm the efficiency of observing the eclipses onboard satellites. 相似文献
959.
A. A. Vostrukhin D. V. Golovin A. S. Kozyrev M. L. Litvak A. V. Malakhov I. G. Mitrofanov M. I. Mokrousov T. M. Tomilina Yu. I. Bobrovnitskiy A. S. Grebennikov M. M. Laktionova B. N. Bakhtin A. V. Sotov 《Cosmic Research》2018,56(3):208-212
The results of testing a number of space-based detectors that contain PMTs or high-voltage electrodes for the noise from the microphonics that occurs in the signal path due to external mechanical action have been presented. A method for the vibration isolation of instruments aboard a spacecraft has been proposed to reduce their responsivity to vibrations. 相似文献
960.
N. Petrova T. Abdulmyanov H. Hanada 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2012
Targets and problems of the future Japanese project ILOM (In situ Lunar Orientation Measurement), which is planned to be realized as one kind of observations of lunar rotation at the second stage of SELENE-2 mission, are briefly described in the article. Inverse problem of lunar physical libration is formulated and solved. Accuracy of libration angles depending on accuracy of measuring selenographic coordinates is estimated. It is shown that selenographic coordinates of polar stars are insensitive to longitudinal librations τ(t). Comparing coordinates calculated for two models of a rigid and deformable Moon is carried out and components sensitive to Love number k2 and to anelastic time delay are revealed. 相似文献