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  • Other Sources  (16)
  • ASTRONOMY
  • Air Transportation and Safety
  • Meteorology and Climatology
  • SPACE RADIATION
  • 1955-1959  (16)
  • 1
    Publication Date: 2011-03-24
    Description: No abstract available
    Keywords: Air Transportation and Safety
    Format: text
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  • 2
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    In:  CASI
    Publication Date: 2012-05-30
    Keywords: SPACE RADIATION
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  • 3
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    In:  CASI
    Publication Date: 2012-06-02
    Keywords: SPACE RADIATION
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  • 4
    Publication Date: 2019-05-10
    Keywords: SPACE RADIATION
    Type: AFOSR-TN-59-769 , AD-227517
    Format: text
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  • 5
    Publication Date: 2019-06-28
    Description: A statistical survey and a preliminary analysis are made of icing data collected from scheduled flights over the United States and Canada from November 1951 to June 1952 by airline aircraft equipped with NACA pressure-type icing-rate meters. This interim report presents information obtained from a continuing program sponsored by the NACA with the cooperation of the airlines. An analysis of over 600 icing encounters logged by three airlines operating in the United States, one operating in Canada and one operating up the coast to Alaska, is presented. The icing conditions encountered provided relative frequencies of many icing-cloud variables, such as horizontal extent, vertical thickness, temperatures, icing rate, liquid-water content, and total ice accumulation. Liquid-water contents were higher than data from earlier research flights in layer-type clouds but slightly lower than previous data from cumulus clouds. Broken-cloud conditions, indicated by intermittent icing, accounted for nearly one-half of all the icing encounters. About 90 percent of the encounters did not exceed a distance of 120 miles, and continuous icing did not exceed 50 miles for 90 percent of the unbroken conditions. Icing cloud thicknesses measured during climbs and descents were less than 4500 feet for 90 percent of the vertical cloud traverses.
    Keywords: Meteorology and Climatology
    Type: NACA-RM-E55F28a
    Format: application/pdf
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  • 6
    Publication Date: 2019-05-10
    Keywords: SPACE RADIATION
    Type: JPL-P-30-21
    Format: text
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  • 7
    Publication Date: 2019-05-10
    Keywords: SPACE RADIATION
    Type: NASA-CR-50742 , SAO SPECIAL REPT.-52
    Format: text
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  • 8
    Publication Date: 2019-05-10
    Keywords: SPACE RADIATION
    Type: JPL/AI-TRANS.-12
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  • 9
    Publication Date: 2019-05-10
    Keywords: SPACE RADIATION
    Type: JPL 30-15
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  • 10
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    In:  Other Sources
    Publication Date: 2019-05-10
    Keywords: SPACE RADIATION
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  • 11
    Publication Date: 2019-06-28
    Description: The tendency for the jet engine rotor to continue to rotate after crash presents the probability that crash-spilled combustibles suspended in the air or puddled on the ground at the engine inlet may be sucked into the engine. Studies with jet engines operating on a test stand and full-scale crashes of turbojet-powered airplanes showed that combustibles drawn into the engine in this way ignite explosively within the engine. Experiment showed that the gas flow through the engine is too rapid to permit the ignition of ingested combustibles on the hot metal in contact with the main gas stream. Ignition will occur on those hot surfaces not in the main gas stream. The portion of the engine airflow is diverted for cooling and ventilation to these zones where the gas moves slowly enough for ignition to occur.
    Keywords: Air Transportation and Safety
    Type: NACA-TR-1363
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  • 12
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    In:  CASI
    Publication Date: 2019-06-27
    Keywords: SPACE RADIATION
    Type: NASA-TT-F-40 , Artificial Earth Satellites, v. 3; 7 p
    Format: text
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  • 13
    Publication Date: 2019-08-17
    Description: A crash-fire protection system to suppress the ignition of crash-spilled fuel that may be ingested by a T-56 turbopropeller engine is described. This system includes means for rapidly extinguishing the combustor flame and means for cooling and inerting with water the hot engine parts likely to ignite engine-ingested fuel. Combustion-chamber flames were extinguished in 0.07 second at the engine fuel manifold. Hot engine parts were inerted and cooled by 52 pounds of water discharged at ten engine stations. Performance trials of the crash-fire prevention system were conducted by bringing the engine up to takeoff temperature, stopping the normal fuel flow to the engine, starting the water discharge, and then spraying fuel into the engine to simulate crash-ingested fuel. No fires occurred during these trials, although fuel was sprayed into the engine from 0.3 second to 15 minutes after actuating the crash-fire protection system.
    Keywords: Air Transportation and Safety
    Type: NASA-MEMO-6-12-59E
    Format: application/pdf
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  • 14
    Publication Date: 2019-08-17
    Description: A crash-fire protection system is described which will suppress the ignition of crash-spilled fuel that may be ingested by a T-56 turbo-propeller engine. This system includes means for rapidly extinguishing the combustor flame, means for cooling and inerting with water the hot engine parts likely to ignite engine ingested fuel, and means for blanketing with bromotrifluoromethane massive metal parts that may reheat after the engine stops rotating. Combustion-chamber flames were rapidly extinguished at the engine fuel nozzles by a fuel shutoff and drain valve. Hot engine parts were inerted and cooled by 42 pounds of water discharged at seven engine stations. Massive metal parts that could reheat were inerted with 10 pounds of bromotrifluoromethane discharged at two engine stations. Performance trials of the crash-fire protection system were conducted by bringing the engine up to takeoff temperature, actuating the crash-fire protection system, and then spraying fuel into the engine to simulate crash-ingested fuel. No fires occurred during these trials, although fuel was sprayed into the engine from 0.3 second to 15 minutes after actuating the crash-fire protection system.
    Keywords: Air Transportation and Safety
    Type: NASA-TN-D-28 , E-308
    Format: application/pdf
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  • 15
    Publication Date: 2019-08-15
    Description: A flight investigation was made to assess the potential operational problems of jet transports in the transonic cruise range. In this study a large multiengine jet airplane having geometric characteristics fairly representative of the jet transport was used; however, in order to ensure general applicability of the results, the aerodynamic characteristics of the test airplane were varied to simulate a variety of jet- transport airplanes. Some of the specific areas investigated include: (1) an overall evaluation of longitudinal stability and control characteristics at transonic speeds, with an assessment of pitch-up characteristics, (2) the effect of buffeting on airplane operational speeds and maneuvering, (3) the desirable lateral-directional damping characteristics, (4) the desirable lateral-control characteristics, (5) an assessment of over-speed and speed-spread requirements, including the upset maneuver, and (6) an assessment of techniques and airplane characteristics for rapid descent and slow-down. The results presented include pilots' evaluation of the various problem areas and specific recommendations for possible improvement of jet-transport operations in the cruising speed range.
    Keywords: Air Transportation and Safety
    Type: NASA-MEMO-3-2-59H
    Format: application/pdf
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  • 16
    Publication Date: 2019-08-16
    Description: Flight studies have been made of the low-speed operational regime of jet transports in order to assess potential operating problems. The study was performed utilizing a large multiengine jet airplane having geometric characteristics fairly representative of the jet transports; however, to insure general applicability of the results, the aerodynamic characteristics of the test airplane were varied to simulate a variety of jet-transport airplanes. The specific areas investigated include those of the take-off and landing, and the relation of these maneuvers to the 1 g stall speed and stalling characteristics. The take-off studies included evaluation of the factors affecting the take-off speed and attitude, including the effects of premature rotation and of over-rotation on ground run required. The approach and landing studies pertained to such factors as: desirable lateral-directional damping characteristics; lateral-control requirements; space-positioning limitations during approach under VFR or IFR conditions and requirements for glide-path controls; and evaluation of factors affecting the pilot's choice of landing speeds. Specific recommendations and some indication of desirable characteristics for the jet transports are advanced to alleviate possible operational difficulties or to improve operational performance in the low-speed range.
    Keywords: Air Transportation and Safety
    Type: NASA-MEMO-3-1-59H , H-103
    Format: application/pdf
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