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  • LUNAR AND PLANETARY EXPLORATION  (125)
  • Aircraft Design, Testing and Performance
  • Aircraft Stability and Control
  • FLUID MECHANICS AND HEAT TRANSFER
  • GENERAL
  • 1980-1984  (180)
  • 1955-1959  (6)
  • 1984  (180)
  • 1958  (6)
Collection
Keywords
Years
  • 1980-1984  (180)
  • 1955-1959  (6)
Year
  • 21
    Publication Date: 2019-06-28
    Description: Although the asteroids are the most plausible candidates for the parent bodies of gas-rich meteorites, dynamical theories have been adduced which favor a cometary origin in certain cases, and some recent studies have indicated that, in the case of gas-rich carbonaceous chondrites, the solar flare irradiation of grains may have occurred prior to the formation of parent bodies. Attention is presently given to advances that have been made in the multidisciplinary studies, encompassing petrography, chemistry, and radiation effects, of the gas-rich meteorites. An evaluation is undertaken of the present understanding of gas-rich meteorite origin and evolution.
    Keywords: LUNAR AND PLANETARY EXPLORATION
    Type: Space Science Reviews (ISSN 0038-6308); 37; 111-159
    Format: text
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  • 22
    Publication Date: 2019-06-28
    Keywords: LUNAR AND PLANETARY EXPLORATION
    Type: Earth, Moon, and Planets (ISSN 0167-9295); 30; 149-173
    Format: text
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  • 23
    Publication Date: 2019-07-13
    Description: Nearly all supersonic V/STOL aircraft concepts are dependent on the thrust deflecting capability of a nozzle. In one unique concept, referred to as the reverse flow dual fan, not only is there a thrust deflecting nozzle for the fan and core engine exit flow, but because of the way the propulsion system operates during vertical takeoff and landing, the supersonic inlet is also used as a thrust deflecting nozzle. This paper presents results of an experimental study to evaluate the performance of a supersonic inlet used as a thrust deflecting nozzle for this reverse flow dual fan concept. Results are presented in terms of nozzle thrust coefficient and thrust vector angle for a number of inlet/nozzle configurations. Flow visualization and nozzle exit flow survey results are also shown.
    Keywords: FLUID MECHANICS AND HEAT TRANSFER
    Type: NASA-TM-83439 , E-1737 , NAS 1.15:83439 , Joint Propulsion Conference; Jun 27, 1983 - Jun 29, 1983; Seattle, WA; United States
    Format: application/pdf
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  • 24
    Publication Date: 2019-07-13
    Description: This paper examines current research efforts underway at Lewis Research Center which have focused on improving the structural durability of the SSME turbodrive system through more fully examining the aerothermodynamics of the flow system. This objective was achieved by developing three-dimensional viscous and inviscid computer codes to predict the pressure and temperature distributions in the engine flow passages, particularly within the SSME turbines and turnaround ducts.
    Keywords: FLUID MECHANICS AND HEAT TRANSFER
    Type: SAE PAPER 841522 , Space systems technology; Oct 15, 1984 - Oct 18, 1984; Long Beach, CA
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  • 25
    Publication Date: 2004-12-03
    Description: Over the last 50 years, aeronautical structures have evolved from the wood, fabric, and wire of low-speed biplanes to supersonic aircraft fabricated with advanced metallic and nonmetallic materials. The advances made in structures technology have had significant impact on aircraft design and performance. An example is the large weight reductions being realized from the utilization of composite materials for secondary and primary structures. However, structural advances have been evolutionary, not revolutionary. Through the year 2000, there are opportunities to obtain significant new advancements in structural technology. These advances could result in considerable performance and capability payoffs such as increased payload, range, speed, maneuverability, fuel efficiency, and safety through reductions in weight, increases in strength, and the ability to make structures pliable. Also, with new manufacturing processes it is possible that reductions in production costs will be realized. Some of the structural technology areas where future major advances could be made are adaptive structures, thermal structures, damage tolerant structures, propulsion system structures, and new structural concepts.
    Keywords: Aircraft Design, Testing and Performance
    Type: Aeronautics Technology Possibilities for 2000: Report of a Workshop; 71-98; NASA-CR-205283
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  • 26
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    In:  CASI
    Publication Date: 2005-08-09
    Keywords: GENERAL
    Type: Notes on Space Technol.; 15 p
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  • 27
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    In:  CASI
    Publication Date: 2005-08-09
    Keywords: GENERAL
    Type: Notes on Space Technol.; 65 p
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  • 28
    Publication Date: 2006-04-06
    Description: The origin of Mars surface units and the extent of subsequent cratering play key roles in determining surface texture. At scale sizes of 0.1-10 meters, however, there is a growing body of evidence that wind is the dominant force. The direct and indirect evidence which implies that meter-scale surface texture on Mars is controlled by the wind is presented. Since radar is uniquely sensitive to structure on these scales, radio wave scattering data can provide insight on aeolian activity available from no other source.
    Keywords: LUNAR AND PLANETARY EXPLORATION
    Type: NASA. Washington Rept. of Planetary Geology Program, 1983; p 273-275
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  • 29
    Publication Date: 2006-04-06
    Description: A photometrically and geometrically reduced data base is being produced for the Galilean Satellites using Voyager Imaging data. The basic data set used is essentially all the useful satellite images returned by Voyager. Each frame was radiometrically calibrated and many are projected into cartographic formats. Mosaics of low, medium and high resolution frames being made for each satellite consist of registered digital images with intensity values scaled through a traceable calibration procedure to normal albedo values. Many of the mosaics are being made in two versions. One version is an albedo version and the second is a maximum discrimination version in which large variations in brightness across the picture are suppressed.
    Keywords: LUNAR AND PLANETARY EXPLORATION
    Type: NASA. Washington Rept. of Planetary Geology Program, 1983; p 259-260
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  • 30
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    In:  CASI
    Publication Date: 2006-04-06
    Description: On the basis of the icy conglomerate model of cometary nuclei, various observations demonstrate the spotted nature of many or most nuclei, i.e., regions of unusual activity, either high or low. Rotation periods, spin axes and even precession of the axes are determined. The observational evidence for variations in activity over the surfaces of cometary nuclei are listed and discussed. On June 11 the comet IRAS-ARAKI-ALCOCK approached the Earth to a distance of 0.031 AU, the nearest since C/Lexell, 1770 I, providing a unique opportunity for near-nucleus observations. Preliminary analysis of these images establishes the spin axis of the nucleus, with an oblioquity to the orbit plane of approximately 50 deg, and a lag angle of sublimation approximately 35 deg from the solar meridian on the nucleus. Asymmetries of the inner coma suggests a crazy-quilt distribution of ices with differing volatility over the surface of the nucleus. The observations of Comet P/Homes 1892 III, exhibiting two 8-10 magnitude bursts, are carefully analyzed. The grazing encounter produced, besides the first great burst, an active area on the nucleus, which was rotating retrograde with a period of 16.3hr and inclination nearly 180 deg. After the first burst the total magnitude fell less than two magnitudes from November 7 to November 30 (barely naked eye) while the nuclear region remained diffuse or complex, rarely if ever showing a stellar appearance. The fading was much more rapid after the second burst. The grazing encounter distributed a volume of large chunks in the neighborhood of the nucleus, maintaining activity for weeks.
    Keywords: LUNAR AND PLANETARY EXPLORATION
    Type: NASA. Washington Repts. of Planetary Geol. Program; p 51-53
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