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  • 1
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    In:  Geophys. J. Int., Hannover, Dt. Geophys. Ges. e. V., vol. 160, no. 3, pp. 855-868, pp. L15S14, (ISSN: 1340-4202)
    Publication Date: 2005
    Keywords: Seismicity ; Crustal deformation (cf. Earthquake precursor: deformation or strain) ; Velocity depth profile ; Rock mechanics ; Plate tectonics ; Earthquake catalog ; Magnitude ; seismic Moment ; Hypocentral depth ; porosity ; Mineralogy ; Rheology ; GJI ; deformation, ; Explorer, ; Juan ; de ; Fuca, ; oceanic ; crust, ; seismicity, ; transform ; faults
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  • 2
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    In:  Seismological Research Letters, Hannover, Dt. Geophys. Ges. e. V., vol. 69, no. 3, pp. 217-221, pp. L15S14, (ISSN: 1340-4202)
    Publication Date: 1991
    Keywords: Nuclear explosion ; Seismology ; Instruments ; Sea seismics
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  • 3
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    In:  Other Sources
    Publication Date: 2011-08-10
    Description: Reduction of pressure differences between back and front of parabolic reflectors by use of a cellular mesh
    Keywords: ELECTRONIC EQUIPMENT
    Format: text
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  • 4
    Publication Date: 2011-08-12
    Description: Plasma temperature and ion concentration profiles determined from simultaneous measurements by Alouette 2 and Explorer 31 satellites of electron density, temperature and ion abundance
    Keywords: GEOPHYSICS
    Type: ; ADEMIE DES SCIENCES
    Format: text
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  • 5
    Publication Date: 2011-08-16
    Description: A simple two-ion model was employed to evaluate the ionospheric effects of various nocturnal ionization sources. The model was used to calculate the decay of the electron number density at 90 km with and without illumination by Scorpius XR-1 X rays. Reflection parameters for the determination of the effect of cosmic x-ray sources on radio wave propagation were also obtained. The results obtained in the investigation do not support the proposal made by Anathakrishnan and Ramanathan (1969) that the X-ray source in Scorpius XR-1 affects the nighttime lower ionosphere of the earth.
    Keywords: GEOPHYSICS
    Type: Journal of Atmospheric and Terrestrial Physics; 37; May 1975
    Format: text
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  • 6
    Publication Date: 2013-08-31
    Description: The Space Infrared Telescope Facility (SIRTF) is planned for launch by NASA in the mid-1990's. It will be a cryogenically-cooled observatory for infrared astronomy and will carry several focal plane instruments which will provide a wide range of imaging, photometric, and spectroscopic capabilities. SIRTF will build on the scientific and technical progress of the successful IRAS mission and take the next step in the exploration of the Universe at infrared wavelengths. Most of the observing time during the five-to-ten year SIRTF mission will be available to General Investigators, so there will be ample opportunities for the pursuit of problems originating from within the Space Life Sciences community. Here, a review is given of the capabilities of SIRTF for this style of investigation, using the study of carbon in the Galaxy as a specific example. The very high sensitivity of SIRTF's spectrometers to diffuse emission will allow studies of carbon in both the gaseous and solid phase in the interstellar medium and should be of particular importance for the identification of the carbon-bearing macromolecules believed to be responsible for the emission features identified in the near infrared. SIRTF will also carry out studies of a wide variety of evolved stars which are returning gas and solid phase carbon to the interstellar medium and contribute to our understanding of the carbon budget in the Galaxy. These studies in the area of galactic astronomy will be complemented by detailed investigations of carbon-bearing compounds in solar system objects, including the surfaces of distant asteroids and cometary nuclei which are too faint to be studied in any other way.
    Keywords: ASTRONOMY
    Type: Carbon in the Galaxy: Studies from Earth and Space; p 287-302
    Format: application/pdf
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  • 7
    Publication Date: 2013-08-31
    Description: Astronomers are lately estimating there are 400,000 Earth visiting asteroids larger than 100 meters in diameter. These asteroids are accessible sources of building materials, propellants, oxygen, water, and minerals which also constitute a huge momentum reserve, potentially usable for travel throughout the solar system. To use this momentum, these stealthy objects must be tracked and the extraction of the momentum wanted must be learned. Momentum harvesting by momentum transfer from asteroid to spacecraft, and by using the momentum of the extraterrestrial material to help deliver itself to the destination are discussed. A net and tether concept is the suggested means of asteroid capture, the basic momentum exchange process. The energy damping characteristics of the tether will determine the velocity mismatch that can be tolerated, and hence the amount of momentum that can be harvested per capture. As it plays out of its reel, drag on the tether steadily accelerates the spacecraft. A variety of concepts for riding and using the asteroid after capture are discussed. The hitchhiker uses momentum transfer only. The beachcomber, the caveman, the swinger, the prospector, and the rock wrecker also take advantage of raw asteroidal materials. The chemist and the hijacker go further, they process the asteroid into propellant. Or, an 'asteroid railway system' could evolve with each hijacked asteroid becoming a scheduled train. Travelers could board the space railway system assured that water, oxygen, and propellants await them.
    Keywords: ASTRONAUTICS (GENERAL)
    Type: NASA. Lewis Research Center, Vision-21: Space Travel for the Next Millennium; p 276-285
    Format: application/pdf
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  • 8
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    In:  Other Sources
    Publication Date: 2019-01-25
    Description: When faced with a variety of technical options to solve a problem, program planners often try to identify one potential winner, then channel their resources into this option. The more scarce their resources are perceived to be, the more likely they are to fall into this trap of illogic. The real ideal solution could well be an optimum combination of options, not just one. Many propulsion opportunities are tantalizing solutions to the potentially high cost of travelling to other planets. Among these opportunities, nuclear thermal rockets (NTR), nuclear electric propulsion (NEP), and asteroid derived propellants stand out as high-payoff modest-challenge options, as near term as they are resolved to be made. But which to choose? Or should higher risk higher payoff technology be opted for, such as fusion? The approach advocated here, technoflex, is one that addresses NTR, NEP, and asteroid propellants in harmony rather than in isolation. Technoflex is technology rich, and option flexible. Technoflex should cost roughly the same as a classic phased technology elimination approach. The synergistic benefits amongst these three options, how they can be efficiently pursued together, and how they can fit with longer range technologies are stressed. Even if no single option reaches its highest expectations, the combinations of any two partial winners would still give big dividends. These combinations are cheap propellants in space, dual mode high thrust/low thrust, or versatile propellant NTR. The triple payoff is excellent, even if all three options would pan out below expectations. If only one option reaches its potential, it could make the other two still worth their investment. If all three options meet full expectations, the triple payoff is a space propulsion jackpot which makes concern about the initial investment ludicrous as well as open up the solar system to expedient exploration.
    Keywords: SPACECRAFT PROPULSION AND POWER
    Type: Arizona Univ., Resources of Near-Earth Space: Abstracts; p 23
    Format: text
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  • 9
    facet.materialart.
    Unknown
    In:  Other Sources
    Publication Date: 2019-01-25
    Description: Astronomers are lately estimating there are 400,000 earth visiting asteroids larger than 100 meters in diameter. These asteroids are uniquely accessible sources of building materials, propellants, oxygen, water, and minerals. They also constitute a huge momentum reserve, potentially usable for travel throughout the solar system. To use this momentum, these stealthy objects must be tracked and the ability to extract the desired momentum obtained. Momentum harvesting by momentum transfer from asteroid to spacecraft, and by using the momentum of the extraterrestrial material to help deliver itself to its destination is discussed. The purpose is neither to quantify nor justify the momentum exchange processes, but to stimulate collective imaginations with some intriguing possibilities which emerge when momentum as well as material is considered. A net and tether concept is the suggested means of asteroid capture, the basic momentum exchange process. The energy damping characteristics of the tether determines the velocity mismatch that can be tolerated, and hence the amount of momentum that can be harvested per capture. As the tether plays out of its reel, drag on the tether steadily accelerates the spacecraft and dilutes, in time, the would-be collision. A variety of concepts for riding and using asteroids after capture are introduced. The hitchhiker uses momentum transfer only. The beachcomber, the caveman, the swinger, the prospector, and the rock wrecker also take advantage of raw asteroid materials. The chemist and the hijacker go further, they process the asteroid into propellants. Or, an asteroid railway system could be constructed with each hijacked asteroid becoming a scheduled train. Travelers could board this space railway system assured that water, oxygen propellants, and shielding await them. Austere space travel could give way to comforts, with a speed and economy impossible without nature's gift of earth visiting asteroids.
    Keywords: ASTROPHYSICS
    Type: Arizona Univ., Resources of Near-Earth Space: Abstracts; p 23
    Format: text
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  • 10
    Publication Date: 2017-06-27
    Description: Runway grooving at Kansas City Municipal Airport
    Keywords: FACILITIES, RESEARCH, AND SUPPORT
    Type: NASA, WASHINGTON PAVEMENT GROOVING AND TRACTION STUDIES 1969; P 301-308
    Format: application/pdf
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