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821.
822.
O.H.库德尔雅绍夫 《航空精密制造技术》1999,35(6)
介绍了俄罗斯大型运载火箭壳体结构的材料。装配和焊接概况.对我国同类型航天火箭的制造有参考和借鉴意义. 相似文献
823.
A. A. Fedorova O. I. Korablev S. Perrier J. -L. Bertaux F. Lefevre A. Rodin A. Kiselev 《Cosmic Research》2006,44(4):294-304
The SPICAM experiment onboard the Mars-Express spacecraft includes sounding the Martian atmosphere in the ultra-violet (118–320 nm) and near IR (1–1.7 μm) ranges. The infrared spectrometer operates in the range of 1–1.7 μm with a resolution of 3.5 cm?1 in the mode of nadir observations and solar and stellar occulations. This paper is devoted to analyzing the basic results of nadir observations of the infra-red SPICAM channel during the first Martian year of the instrument operation: from January 2004 to November 2005. One of the primary goals of SPICAM-IR is water vapor monitoring in the atmosphere of Mars in the band of 1.37 μm and ozone abundance determination from the day-time airglow of molecular oxygen O2(a 1Δg) in the band of 1.27 μm. Simultaneous measurements of these minor constituents of the planet are necessary for understanding photochemical processes in the Martian atmosphere. The degree of their anticorrelation and a comparison with the results of photochemical modeling of the atmosphere will contribute to our knowledge of the Martian atmosphere stability. 相似文献
824.
Growing complexity of some technological systems requires engineering assurance that the systems will perform effectively at some distant point in time, when all contractual requirements shall have been met and the first assembled system faces the performance test program. The many new- and old-related assurance disciplines are outlined briefly, as being indispensable to effective engineering acquisition of present day systems of large magnitude for civilian or defense purposes. 相似文献
825.
We study the design of constant false-alarm rate (CFAR) tests for detecting a rank-one signal in the presence of background Gaussian noise with unknown spatial covariance. We look at invariant tests, i.e., those tests whose performance is independent of the nuisance parameters, like the background noise covariance. Such tests are shown to have the desirable CFAR property. We characterize the class of all such tests by showing that any invariant decision statistic can be written as a function of two basic statistics which are in fact the adaptive matched filter (AMF) statistic and Kelly's generalized likelihood ratio statistic. Further, we establish an optimum test in the limit of low signal-to-noise ratio (SNR), the locally most powerful invariant (LMPI) test. We also derive the bound for the probability of detection of any invariant detector, at a fixed false-alarm rate, and compare the LMPI and the published detectors (Kelly and AMF) to it 相似文献
826.
Two NASA laser satellite tracking systems on opposite sides of the San Andreas fault will be used in an experiment to measure the gross relative motion of the tectonic plates of North America and the Pacific during the next several years. Initial sites at San Diego on the Pacific Plate and Quincy, California, on the North American Plate, nearly 900 km apart, have already been selected and occupied, and other sites further south are proposed. Each site is occupied for two or three months per year and simultaneous precision laser distance measurements to the Beacon Explorer-C satellite from these sites will be used to determine the relative position of one site with respect to the other. Results of a simulation of this experiment in which a pair of sites are reoccupied annually for about eight years indicate an eventual accuracy of about 0.5 cm/yr in the average plate motion. The results of a preliminary three-month observing period in 1972 indicate a precision of about 15 cm in the chord distance between the San Diego and Quincy sites. 相似文献
827.
R. L. Aptekar D. D. Frederiks S. V. Golenetskii V. N. Ilynskii E. P. Mazets V. N. Panov Z. J. Sokolova M. M. Terekhov L. O. Sheshin T. L. Cline D. E. Stilwell 《Space Science Reviews》1995,71(1-4):265-272
The Konus-W experiment to be flown on board the GGS-Wind spacecraft is designed to observe gamma-ray bursts and solar flares with moderate spectral and high time resolution. Two large scintillators are used to provide omnidirectional sensitivity. The primary scientific objectives are the study of the continuum energy spectra and spectral features of these events in the energy range of 10 keV to 10 MeV, as well as their time histories in soft, medium, and hard energy bands, with a time resolution to 2 ms. 相似文献
828.
C. Feiler M. Buser E. Kajari W. P. Schleich E. M. Rasel R. F. O’Connell 《Space Science Reviews》2009,148(1-4):123-147
In the present paper we follow three major themes: (i) concepts of rotation in general relativity, (ii) effects induced by these generalized rotations, and (iii) their measurement using interferometry. Our journey takes us from the Foucault pendulum via the Sagnac interferometer to manifestations of gravito-magnetism in double binary pulsars and in Gödel’s Universe. Throughout our article we emphasize the emerging role of matter wave interferometry based on cold atoms or Bose–Einstein condensates leading to superior inertial sensors. In particular, we advertise recent activities directed towards the operation of a coherent matter wave interferometer in an extended free fall. 相似文献
829.
N. I. Mikheev V. M. Molochnikov I. A. Davletshin O. A. Dushina 《Russian Aeronautics (Iz VUZ)》2009,52(1):77-82
A method for simulating spatial-temporary characteristics of pulsating flows in the varying-in-length-area channels based on the solution of one-dimensional nonstationary equations of gas dynamics is presented. The calculation results are compared with the experimental data, and it is shown that the method being proposed rather adequately simulates real processes in complex unsteady flows. 相似文献
830.
The purpose of this paper is to introduce a new method in the research of radiative and thermal properties of materials with further applications in the design of thermal control systems (TCS) of spacecrafts. In this paper the radiative and thermal properties (emissivity and thermal conductance) of a multilayered thermal-insulating blanket (MLI), which is a screen-vacuum thermal insulation as a part of the TCS for perspective spacecrafts, are estimated. Properties of the materials under study are determined in the result of temperature and heat flux measurement data processing based on the solution of the inverse heat transfer problem (IHTP) technique. Given are physical and mathematical models of heat transfer processes in a specimen of the multilayered thermal-insulating blanket located in the experimental facility. A mathematical formulation of the inverse heat conduction problem is presented as well. The practical approves were made for specimen of the real MLI. 相似文献