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  • FACILITIES, RESEARCH, AND SUPPORT  (2)
  • AIRCRAFT DESIGN, TESTING AND PERFORMANCE  (1)
  • COMMUNICATIONS  (1)
  • 1
    facet.materialart.
    Unbekannt
    In:  Other Sources
    Publikationsdatum: 2011-08-18
    Beschreibung: The aerodynamic characteristics which affect the fuel consumption of general aviation aircraft are outlined. All data are presented in the form of graphs.
    Schlagwort(e): AIRCRAFT DESIGN, TESTING AND PERFORMANCE
    Materialart: NASA. Langley Research Center Joint Univ. Program for Air Transportation Res., 1980; p 133-142
    Format: text
    Standort Signatur Erwartet Verfügbarkeit
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  • 2
    Publikationsdatum: 2019-06-27
    Beschreibung: Theoretical analysis and experimental data are combined to yield the errors to be used with antenna gain, antenna patterns, and RF cable insertion loss measurements for the Mariner Venus-Mercury 1973 Flight Project. These errors apply to measurements conducted at the JPL Mesa, West Antenna Range, on the high gain antenna, low gain antenna, and RF coaxial cables.
    Schlagwort(e): COMMUNICATIONS
    Materialart: NASA-CR-133230 , JPL-TM-33-625
    Format: application/pdf
    Standort Signatur Erwartet Verfügbarkeit
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  • 3
    facet.materialart.
    Unbekannt
    In:  CASI
    Publikationsdatum: 2019-06-27
    Beschreibung: A low cost air mass 2 solar simulator for testing flat-plate solar collectors was developed and operated at Lewis. Total cost was less than $10,800/sq m ($1000/sq ft). It consists of an array of 143 tungsten-halogen 300-watt lamps, each having integral dichroic coated reflectors. A second array of 143 respective hexagonal-shaped plastic Fresnel lenses are located approximately 1 focal length from the lamps. The simulator will produce a uniform collimated beam covering an area of 1.2 by 1.2m(4 by 4 ft). Design features, construction details, and component costs are given, as well as measured results on a 12-lamp prototype.
    Schlagwort(e): FACILITIES, RESEARCH, AND SUPPORT
    Materialart: NASA-TM-X-3059 , E-7885
    Format: application/pdf
    Standort Signatur Erwartet Verfügbarkeit
    BibTip Andere fanden auch interessant ...
  • 4
    Publikationsdatum: 2019-07-13
    Beschreibung: Simulation techniques to remove gimbal bearing looseness effect on frequency response and cross axis coupling of Saturn control system S-4B stage
    Schlagwort(e): FACILITIES, RESEARCH, AND SUPPORT
    Materialart: NATIONAL SYMPOSIUM ON SATURN V/APOLLO AND BEYOND; Jun 11, 1967 - Jun 14, 1967; HUNTSVILLE, AL
    Format: text
    Standort Signatur Erwartet Verfügbarkeit
    BibTip Andere fanden auch interessant ...
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