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211.
Jonathan G. Metts James A. Nabity David M. Klaus 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2011
Variable emissivity electrochromics have been proposed as an enabling technology for integrating a radiator capability into a space suit in order to augment or replace the traditional means of heat rejection achieved via water sublimation. Thermal analysis was performed to establish design trade spaces and to provide operational guidelines and performance specifications for electrochromic technology development. Based on using the available surface area of an entire space suit as a radiator and the projected infrared emissivity modulation capability of state-of-the-art electrochromic material, the proposed application for space suit heat rejection suggests the potential exists to reduce or eliminate reliance on water consumption for thermal control within a defined range of metabolic and environmental boundary conditions. 相似文献
212.
A review of global satellite-derived snow products 总被引:1,自引:0,他引:1
Allan Frei Marco Tedesco Shihyan Lee James Foster Dorothy K. Hall Richard Kelly David A. Robinson 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2012
Snow cover over the Northern Hemisphere plays a crucial role in the Earth’s hydrology and surface energy balance, and modulates feedbacks that control variations of global climate. While many of these variations are associated with exchanges of energy and mass between the land surface and the atmosphere, other expected changes are likely to propagate downstream and affect oceanic processes in coastal zones. For example, a large component of the freshwater flux into the Arctic Ocean comes from snow melt. The timing and magnitude of this flux affects biological and thermodynamic processes in the Arctic Ocean, and potentially across the globe through their impact on North Atlantic Deep Water formation. 相似文献
213.
214.
Steven C. Gustafson Evan A. James Andrew J. Terzuoli Jr. Lindsay N. Weidenhammer Rod I. Barnes 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2009
A practical technique for characterizing non-Gaussian radar clutter is specified and demonstrated using Over The Horizon Radar (OTHR) data, as an example. The technique employs maximum likelihood to fit the probability density of the clutter amplitude returns to a mixture of two Rayleigh probability densities instead of the single Rayleigh density typically used for Gaussian clutter. This model for non-Gaussian clutter is fully specified for any set of clutter amplitudes by a log likelihood, two Rayleigh parameters, and a mixing coefficient. A 3D plot of these values yields an easily-visualized clutter characterization, as is illustrated using OTHR data. This technique is a demonstration of clutter characterization using OTHR data, but the method can be applied to characterize other types of clutter data. 相似文献
215.
Jyri Näränen James Carpenter Hannu Parviainen Karri Muinonen George Fraser Marko Peura Aki Kallonen 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2009
Laboratory measurements are presented to study the effects of the physical properties of regolith on planetary soft X-ray fluorescence spectroscopy. Two laboratory setups are used to independently measure these regolith effects using lunar regolith analog samples with three different particle-size ranges. Discussion is given on the data analysis. Some of the data may be valid only for qualitative conclusions. Analytical modelling is used to separate the effects expected for a plane-parallel and homogeneous medium from those of measured regolith analogs. The surface roughness and porosity of the regolith are observed to induce an enhancement of the higher-energy part of the spectrum as a function of the incidence angle. The enhancement is larger for rougher surfaces. A brief discussion is given on the relevance of this study for future planetary missions carrying soft X-ray spectrometers. 相似文献
216.
217.
James E. Richardson H. Jay Melosh Natasha A. Artemeiva Elisabetta Pierazzo 《Space Science Reviews》2005,117(1-2):241-267
The cratering event produced by the Deep Impact mission is a unique experimental opportunity, beyond the capability of Earth-based
laboratories with regard to the impacting energy, target material, space environment, and extremely low-gravity field. Consequently,
impact cratering theory and modeling play an important role in this mission, from initial inception to final data analysis.
Experimentally derived impact cratering scaling laws provide us with our best estimates for the crater diameter, depth, and
formation time: critical in the mission planning stage for producing the flight plan and instrument specifications. Cratering
theory has strongly influenced the impactor design, producing a probe that should produce the largest possible crater on the
surface of Tempel 1 under a wide range of scenarios. Numerical hydrocode modeling allows us to estimate the volume and thermodynamic
characteristics of the material vaporized in the early stages of the impact. Hydrocode modeling will also aid us in understanding
the observed crater excavation process, especially in the area of impacts into porous materials. Finally, experimentally derived
ejecta scaling laws and modeling provide us with a means to predict and analyze the observed behavior of the material launched
from the comet during crater excavation, and may provide us with a unique means of estimating the magnitude of the comet’s
gravity field and by extension the mass and density of comet Tempel 1. 相似文献
218.
Brian J. Anderson Mario H. Acuña David A. Lohr John Scheifele Asseem Raval Haje Korth James A. Slavin 《Space Science Reviews》2007,131(1-4):417-450
The Magnetometer (MAG) on the MErcury Surface, Space ENvironment, GEochemistry, and Ranging (MESSENGER) mission is a low-noise,
tri-axial, fluxgate instrument with its sensor mounted on a 3.6-m-long boom. The boom was deployed on March 8, 2005. The primary
MAG science objectives are to determine the structure of Mercury’s intrinsic magnetic field and infer its origin. Mariner
10 observations indicate a planetary moment in the range 170 to 350 nT R
M3 (where R
M is Mercury’s mean radius). The uncertainties in the dipole moment are associated with the Mariner 10 trajectory and variability
of the measured field. By orbiting Mercury, MESSENGER will significantly improve the determination of dipole and higher-order
moments. The latter are essential to understanding the thermal history of the planet. MAG has a coarse range, ±51,300 nT full
scale (1.6-nT resolution), for pre-flight testing, and a fine range, ±1,530 nT full scale (0.047-nT resolution), for Mercury
operation. A magnetic cleanliness program was followed to minimize variable and static spacecraft-generated fields at the
sensor. Observations during and after boom deployment indicate that the fixed residual field is less than a few nT at the
location of the sensor, and initial observations indicate that the variable field is below 0.05 nT at least above about 3 Hz.
Analog signals from the three axes are low-pass filtered (10-Hz cutoff) and sampled simultaneously by three 20-bit analog-to-digital
converters every 50 ms. To accommodate variable telemetry rates, MAG provides 11 output rates from 0.01 s−1 to 20 s−1. Continuous measurement of fluctuations is provided with a digital 1–10 Hz bandpass filter. This fluctuation level is used
to trigger high-time-resolution sampling in eight-minute segments to record events of interest when continuous high-rate sampling
is not possible. The MAG instrument will provide accurate characterization of the intrinsic planetary field, magnetospheric
structure, and dynamics of Mercury’s solar wind interaction. 相似文献
219.
Nucleosynthesis in the standard hot big bang cosmology offers a successful account of the production of the light nuclides during the early evolution of the Universe. Consistency among the predicted and observed abundances of D,3He,4He and7Li leads to restrictive lower and upper bounds to the present density of nucleons. In particular, the upper bound ensures that nucleons cannot account for more than a small fraction (<0.06h
50
–2
) of the mass in a critical density (Einstein-de Sitter) Universe. In contrast, x-ray observations of rich clusters of galaxies suggest strongly that baryons (in hot gas) contribute a significant fraction of the total cluster mass (0.2h
50
–3/2
). If, indeed, clusters do provide a fair sample of the mass in the Universe, this crisis forces us to consider other ways of mitigating it, including the politically incorrect possibility that <1. The options, including magnetic or turbulent pressure, clumping and non-zero space curvature and/or cosmological constant, are discussed. 相似文献
220.
Operational life improvement of SSME high-pressure turbopumps 总被引:1,自引:0,他引:1
The current Space Shuttle Main Engine Phase I engine has demonstrated excellent flight performance at power levels up to 104% of rated power level. Early certification testing at 109% power level showed the operational life of the high pressure turbopumps to be limited. A development program, Phase II, has been under way since 1983 to increase the operational life and provide additional margin. The history of the SSME Phase I engine and the design and results of the SSME Phase II Program are presented. Operational life limits and high-maintenance areas of the high-pressure turbopumps are identified. The Phase II design improvements, supporting analyses, and test results are described. The formal certification test program is discussed. Modifications have been made to the high-pressure fuel turbopump to reduce turbine operating temperature, to extend the life of the first- and second-stage turbine blades, and to reduce sheet metal maintenance. Modifications have been made to the high-pressure oxidizer turbopump to improve bearing life and to eliminate subsynchronous whirl. These are discussed in detail, as is the design and use of special instrumentation to provide for rapid evaluation of merit. 相似文献